In this section we give the complete formulation for TB model ...Document Transcript
RSS Tech. Proposal 121599A-1 Revised:
November 2, 2000
Algorithm Theoretical Basis Document
AMSR Ocean Algorithm
Principal Investigator: Frank J. Wentz
Co-Investigator: Thomas Meissner
Goddard Space Flight Center
National Aeronautics and Space Administration
Greenbelt, MD 20771
Table of Contents
1. Overview and Background Information 1
1.1. Introduction 1
1.2. Objectives of Investigation 2
1.3. Approach to Algorithm Development 2
1.4. Algorithm Development Plan 3
1.5. Concerns Regarding Sea-Surface Temperature Retrieval 3
1.6. Historical Perspective 5
1.7. AMSR Instrument Characteristics 7
2. Geophysical Model for the Ocean and Atmosphere 10
2.1. Introduction 10
2.2. Radiative Transfer Equation 10
2.3. Model for the Atmosphere 13
2.4. Dielectric Constant of Sea-Water and the Specular Sea Surface 20
2.5. The Wind-Roughened Sea Surface 23
2.6. Atmospheric Radiation Scattered by the Sea Surface 28
2.7. Wind Direction Effects 29
3. The Ocean Retrieval Algorithm 31
3.1. Introduction 31
3.2. Multiple Linear Regression Algorithm 31
3.3. Derivation and Testing of the Linear Regression Algorithm 32
3.4. Non-Linear, Iterative Algorithm 36
3.5. Post-Launch In-Situ Regression Algorithm 38
3.6. Incidence Angle Variations 39
4. Level-2 Data Processing Issues 40
4.1. Retrievals at Different Spatial Resolutions 40
4.2. Granules and Metadata 43
4.3. Requirements for Ancillary Data Sets 44
4.4. Computer Resources and Programming Standards 45
5. Validation for the Ocean Products Suite 46
5.1. Introduction 46
5.2. Sea-Surface Temperature Validation 47
5.3. Wind Speed Validation 49
5.4. Water Vapor Validation 50
5.5. Cloud Water Validation 52
6. References 55
List of Figures
1. Development steps for ocean algorithm 4
2. Block diagram for PM AMSR feedhorns and radiometers 9
3. The atmospheric absorption spectrum for oxygen, water vapor,… 15
4. The effective air temperature TD for downwelling radiation… 17
5. Derivation and testing of the linear regression algorithm 33
6. Preliminary results for the linear statistical regression algorithm… 35
7. Data processing flow for ocean algorithm 41
8. Locations of data buoys 49
9. Radiosonde stations on small islands 52
10. Probability density functions (pdf) for liquid cloud water 54
List of Tables
1. Expected retrieval accuracy for the ocean products 1
2. Comparison of past and future satellite radiometer systems 2
3. Instrument specifications for PM AMSR 8
4. Model coefficients for the atmosphere 18
5. RMS error in oxygen and water vapor absorption approx… 18
6. Coefficients for rayleigh absorption 20
7. Model coefficients for geometric optics 27
8. The coefficients m1 and m2 … 28
9. Preliminary estimate of retrieval error 36
10. AMSR level-2 ocean data record 43
11. Ancillary data sets required by level-2 ocean algorithm 44
12. Some of the available SST products 47
13. NDBC moored buoy open water locations as of July 1996 48
14. Island radiosonde station locations as of September 1996 51
List of Symbols
Symbol Definition Units
aO1, aO2 coefficients for oxygen absorption see Table 4
aV1, aV2 coefficients for water vapor absorption see Table 4
aL1, aL2 coefficients for liquid water absorption see Table 6
A the A-matrix relating Y to X arbitrary
AO vertically integrated oxygen absorption naper
AV vertically integrated water vapor absorption naper
AL vertically integrated cloud liquid water absorption naper
b0 to b7 coefficients for effective air temperature see Table 4
c speed of light cm/s
C chlorinity of sea water parts/thousand
E sea-surface emissivity none
f fractional foam coverage none
F foam+diffraction factor for sea-surface reflectivity none
h Planck’s constant in eq. (2) erg-s
h height above Earth surface, elsewhere cm
h0 surface roughness length cm
hi, hs h-pol vectors for incident and scattered radiation none
Iλ specific intensity erg/s-cm3-ster
j −1 none
k Boltzmann’s constant erg/K
ki upward unit propagation vector none
ks downward unit propagation vector none
L vertically integrated cloud liquid water mm
m1 , m2 coefficients for foam+diffraction factor s/m
n unit normal vector for tilted surface facet none
P column vector of geophysical parameters varies
P(Su,Sc) probability density function of surface slope none
Pλ specific power erg/s
p unit polarization vector none
Symbol Definition Units
r0 to r3 coefficients for geometric optics see Table 7
R total sea-surface reflectivity none
R0 specular reflectivity none
Rclear foam-free sea-surface reflectivity none
Rgeo geometric optics sea-surface reflectivity none
R× reflectivity of secondary intersection none
s path length in Section 2.2 cm
s salinity, elsewhere parts/thousand
S total path length through atmosphere cm
Sc crosswind slope for tilted surface facet none
Su upwind slope for tilted surface facet none
tS sea-surface temperature Celsius
T temperature K
TB brightness temperature K
TBU upwelling atmospheric brightness temperature K
TBD downwelling atmospheric brightness temperature K
TBΩ sky radiation scattered upward by Earth surface K
TB↑ upwelling surface brightness temperature K
TB↓ downwelling cold space brightness temperature K
TC cold space brightness temperature K
TD effective temperature for downwelling radiation K
TE effective temperature of surface+atmosphere K
TS sea-surface temperature K
TU effective temperature for upwelling radiation K
TV typical sea temperature for given water vapor K
vi, vs v-pol vectors for incident and scattered radiation none
V vertically integrated water vapor mm
W wind speed 10 m above sea surface m/s
X column input vector arbitrary
Y column output vector arbitrary
~ measurement vector arbitrary
Symbol Definition Units
α total absorption coefficient naper/cm
αO oxygen absorption coefficient naper/cm
αV water vapor absorption coefficient naper/cm
αL cloud liquid water absorption coefficient naper/cm
β diffraction factor for sea-surface reflectivity none
γ coefficients for wind direction variation of E none
∆S2 total slope variance of sea surface none
ε TB measurement error in Section 3 K
ε complex dielectric constant of water, elsewhere none
ε∞ dielectric constant at infinite frequency none
εS static dielectric constant of sea water none
εS0 static dielectric constant of distilled water none
εφ error in specifying wind direction degree
εTs error in specifying sea-surface temperature K
θi incidence angle degree
θs zenith angle degree
κ reduction in sea-surface reflectivity due to foam none
ϕi azimuth angle for ki degree
ϕs azimuth angle for ks degree
φ wind direction relative to azimuth look direction degree
λ radiation wavelength cm
λR relaxation wavelength of sea water cm
λR0 relaxation wavelength of distilled water cm
µ change in TB w.r.t. incidence angle K/degree
η spread factor for relaxation wavelengths none
Ω fit parameter for sea surface scattering integral none
Ξ error correlation matrix arbitrary
ρh h-pol Frensel reflection coefficient none
ρv v-pol Frensel reflection coefficient none
ρL liquid water density g/cm3
ρV water vapor density g/cm3
Symbol Definition Units
ρo density of water g/cm3
σ ionic conductivity of sea water s-1
σo,c co-pol. normalized radar cross section none
σo,× cross-pol. normalized radar cross section none
τ atmospheric transmission none
ν radiation frequency GHz
χ shadowing function none
n correction for effective air temperature K
ℑ linearizing function for TB’s none
ℜ linearizing function for geophysical parameters none
1. Overview and Background Information
With the advent of well-calibrated satellite microwave radiometers, it is now possible to
obtain long time series of geophysical parameters that are important for studying the global
hydrologic cycle and the Earth's radiation budget. Over the world's oceans, these radiome-
ters simultaneously measure profiles of air temperature and the three phases of atmospheric
water (vapor, liquid, and ice). In addition, surface parameters such as the near-surface wind
speed, the sea-surface temperature, and the sea ice type and concentration can be retrieved.
A wide variety of hydrological and radiative processes can be studied with these measure-
ments, including air-sea and air-ice interactions (i.e., the latent and sensible heat fluxes, fresh
water flux, and surface stress) and the effect of clouds on radiative fluxes. The microwave
radiometer is truly a unique and valuable tool for studying our planet.
This Algorithm Theoretical Basis Document (ATBD) focuses on the Advanced Mi-
crowave Scanning Radiometer (AMSR) that is scheduled to fly in December 2000 on the
NASA EOS-PM1 platform. AMSR will measure the Earth’s radiation over the spectral
range from 7 to 90 GHz. Over the world’s oceans, it will be possible to retrieve the four im-
portant geophysical parameters listed in Table 1. The rms accuracies given in Table 1 come
from past investigations and on-going simulations that will be discussed. Rainfall can also
be retrieved, which is discussed in a separate AMSR ATBD.
We are confident that the expected retrieval accuracies for wind, vapor, and cloud will be
achieved. The Special Sensor Microwave Image (SSM/I) and the TRMM microwave imager
(TMI) have already demonstrated that these accuracies can be obtained. The AMSR wind
retrievals will probably be more accurate than that of SSM/I and less affected by atmospher-
ic moisture. A comparison between sea surface temperatures (SST) from TMI with buoy
measurements indicate an rms accuracy between 0.5 and 0.7 K. One should keep in mind
that part of the error arises from the temporal and spatial mismatch between the buoy mea-
surement and the 50 km satellite footprint. Furthermore, the satellite is measuring the tem-
perature at the surface the ocean (about 1 mm deep) whereas the buoy is measuring the bulk
temperature near 1 m below the surface. There are still some concerns with regards to the
sea-surface temperature retrieval, which are discussed in Section 1.5.
This document is version 2 of the AMSR Ocean Algorithm ATBD. The primary difference
between this version and the earlier version is that the emissivity model for the 10.7 GHz has
been updated using data from TMI. In addition, there are several small updates to the radia-
tive transfer model (RTM).
Table 1. Expected Retrieval Accuracy for the Ocean Products
Geophysical Parameter Rms Accuracy
Sea-surface temperature TS 0.5 K
Near-surface wind speed W 1.0 m/s
Vertically integrated (i.e., columnar) water vapor V 1.0 mm
Vertically integrated cloud liquid water L 0.02 mm
1.2. Objectives of Investigation
There are two major objectives of this investigation. The first is to develop an ocean re-
trieval algorithm that will retrieve TS, W, V, and L to the accuracies specified in Table 1.
These products will be of great value to the Earth science community. The second objective
is to improve the radiative transfer model (RTM) for the ocean surface and non-raining at-
mosphere. The 6.9 and 10.7 GHz channels on AMSR will provide new information on the
RTM at low frequencies. Experience has shown that these two objectives are closely linked.
A better understanding of the RTM leads to more accurate retrievals. A better understanding
of the RTM also leads to new remote sensing techniques such as using radiometers to mea-
sure the ocean wind vector.
1.3. Approach to Algorithm Development
Radiative transfer theory provides the relationship between the Earth’s brightness tem-
perature TB (K) as measured by AMSR and the geophysical parameters T S, W, V, and L.
This ATBD addresses the inversion problem of finding TS, W, V, and L given TB. We place
a great deal of emphasis on developing a highly accurate RTM. Most of our AMSR work
thus far has been the development and refinement of the RTM. This work is now completed,
and Section 2 describes the RTM in considerable detail.
The importance of the RTM is underscored by the fact that AMSR frequency, polariza-
tion, and incidence angle selection is not the same as previous satellite radiometers. Table 2
compares AMSR with other radiometer systems. Albeit some of the differences are small,
they are still significant enough to preclude developing AMSR algorithms by simply using
existing radiometer measurements. The differences in frequencies and incidence angle must
be taken into account when developing AMSR algorithms.
Table 2. Comparison of Past and Future Satellite Radiometer Systems
Radiometer Frequencies/Polarization Inc. Angle
SeaSat SMMR 6.6VH 10.7VH 18.0VH 21.0VH 37.0VH 49°
Nimbus-7 SMMR 6.6VH 10.7VH 18.0VH 21.0VH 37.0VH 51°
SSM/I 19.3VH 22.2V 37.0VH 85.5VH 53°
TRMM TMI 10.7VH 19.3VH 21.0VH 37.0VH 85.5VH 53°
PM AMSR 6.9VH 10.7VH 18.7VH 23.8VH 36.5VH 89.0VH 55°
Our approach uses the existing radiometer measurements to calibrate various components
of the RTM. The RTM formulation then provides the means to compute T B at any frequency
in the 1-100 GHz range and at any incidence angle in the 50°-60° range. For the SSM/I fre-
quencies and incidence angle, the resulting RTM is extremely accurate. It is able to repro-
duce the SSM/I TB to a rms accuracy of about 0.6 K. (This figure comes from Table 3 in
Wentz , and represents the rms difference between the RTM and SSM/I observations
after subtracting out radiometer noise and in situ inter-comparison errors.) As one moves
away from the SSM/I frequencies and incidence angle, we do expect some degradation in the
RTM accuracy. However, the hope is that the physics of the RTM is reliable enough so that
this degradation is minimal when we interpolate/extrapolate to the AMSR configuration.
Given an accurate and reliable RTM, geophysical retrieval algorithms can be developed.
We are developing in parallel two types of algorithms: the linear regression algorithm and
the non-linear, iterative algorithm. Section 3 discusses each type of algorithm. For both
types, the algorithm development is based on a simulation in which brightness temperatures
for a wide variety of ocean scenes are produced by the RTM. These simulated T B’s then
serve as both a training set and a test set for the algorithms. We have tested this simulation
methodology by developing algorithms for SSM/I. These SSM/I algorithms are then tested
using actual measurements. The results show that the SSM/I algorithms coming from the
RTM simulation have essentially the same performance as those developed directly from
SSM/I measurements. These results are not surprising since the RTM was calibrated to re-
produce the SSM/I TB’s. This exercise is more of a closure verification of the techniques be-
ing used. Simulation results for the AMSR retrieval algorithm are given in Section 3.
1.4. Algorithm Development Plan
Figure 1 shows the basic steps in developing the AMSR ocean algorithm. We are current-
ly developing the version 2 algorithm which includes well-calibrated 10.7-GHz ocean obser-
vations from TMI. The recent TMI results show T S can be accurately retrieved in warm water
above 15°C. We expect even better performance from AMSR because of the additional 6.9
GHz channel, which provides TS sensitivity in cold water. One concern is the variation of the
6.9 and 10.7-GHz TB with wind direction. Wind direction variability may be the dominate
source of error in the TS retrieval if the TB wind direction signal is large. We are currently
studying the TB wind direction effect in considerable detail using a combination of SSM/I,
TMI and collocated buoy observations.
We originally planed to use the AMSR aboard the ADEOS-2 spacecraft to develop and
test the AMSR-E ocean algorithm. Now that the ADEOS-2 launch date has slipped to 2001,
this is no longer possible. We are placing more attention on the TMI data set for AMSR al-
gorithm development. However, the final specification of the 6.9 GHz emissivity will need
to be done after the AMSR-E launch. We expect that the 6.9 GHz emissivity can be relative-
ly quickly specified given 1 to 3 months of AMSR observations.
1.5. Concerns Regarding Sea-Surface Temperature Retrieval
The capability of measuring sea-surface temperature TS through clouds has long been a
goal of microwave radiometry. A global TS product unaffected by clouds and aerosols
would be of great benefit to both the scientific and commercial communities. AMSR will be
the first satellite sensor to furnish this product, provided that certain requirements are met.
Calibrate Radiative Transfer Model (RTM)
using SSM/I and SeaSat SMMR observations
Development first version of AMSR algorithm
using simulated TB's computed by RTM
Version 1 Pre-Launch AMSR Algorithm
Use TRMM results to specify
TRMM parameters at 10.7 GHz
Version 2 Pre-Launch AMSR Algorithm
Final Prelaunch Testing
Final Prelaunch AMSR Algorithm for EOS PM
Specify the Sea Surface Emissivity at 6.9 GHz
Using Actual On-Orbit AMSR Observations
Version 1 Post-Launch AMSR Algorithm
Fig. 1. Development steps for ocean algorithm
The retrieval of sea-surface temperature to an accuracy of 0.5 K requires the following:
1. Radiometer noise for the 6.9V channel be about 0.1K
2. Incidence angle be known to an accuracy of 0.05°
3. Radio frequency interference (RFI) be less than 0.1 K.
4. The retrieval algorithm be able to separate wind effects from TS effects
The first two conditions will be satisfied if the AMSR instrument specifications are met.
The radiometer noise figure for one 6.9 GHz observation is 0.3 K. However, the 6.9 GHz
observations are greatly over sampled. Observations are taken every 10 km, but the spatial
resolution of the footprint is 58 km. During the Level-2A processing, adjacent observations
are averaged together in such a way as to reduce the noise to 0.1 K. In doing this averaging,
the spatial resolution is degraded by only 2%. The pointing knowledge for the PM platform
should be sufficient to meet the incidence angle requirement, as is discussed in Section 3.6.
The last two conditions are our major concern. The band from 5.9 to 7.8 GHz is allocated
to various communication links. The possibility exists that the sidelobe transmissions from
these links will contaminate the AMSR 6.9 GHz measurements. Clearly, this problem needs
more attention. A survey of relevant communication links need to be made and sidelobe
contamination calculations need to be done.
From an algorithm standpoint, the most difficult part of the TS retrieval is separating the
TS signal from the wind signal. The T B wind signal is due to both wind speed and wind di-
rection variations. It is relatively easy to distinguish wind speed variations from a TS varia-
tion. Wind speed mostly affects the h-pol channel and TS mostly affects the v-pol channel.
Thus the polarization signature of the observations provides the means to separate T S from
W. However, wind direction variations are more problematic in that both polarizations are
affected. Simulations (see Section 3) show that without (with) wind direction variability, the
TS retrieval error is 0.3 (0.6). These results are contingent on the assumed amplitude for the
wind directional TB signal at 6.9 GHz. If the wind direction variation proves to be a domi-
nant error source, then we will need to make a correction to the TS retrieval based on some
wind direction database, as is discussed in Section 4.3.
Note that in contrast to IR retrieval techniques, the atmospheric interference at 6.9 GHz is
very small and easily removed using the higher frequency channels, except when there is
rain. And, observations affected by rain are easily detected and can be discarded. Thus, the
atmosphere does not pose a problem for the TS retrieval.
1.6. Historical Perspective
In the 1960’s, it was first recognized that microwave radiometers had the ability to mea-
sure atmospheric water vapor V and cloud liquid water L [Barret and Chung, 1962; Staelin;
1966]. In 1972, Nimbus-5 satellite was launched. Aboard Nimbus-5 was the Nimbus-E Mi-
crowave Spectrometer (NEMS), which had channels at 22.235 and 31.4 GHz. Staelin et al.
 and Grody  demonstrated that water vapor and cloud water could indeed be re-
trieved from the NEMS TB’s. In these retrievals they ignored the effect of wind at the ocean
surface; at these frequencies the effect of TS is minimal.
In the years preceding the launch of Nimbus-5, there were several developments con-
cerning the effect of wind at the ocean's surface. Stogryn  developed a theory to ac-
count for the wind-induced roughness, and Hollinger  made some radiometric mea-
surements from a fixed tower to test the theory. He removed the most obvious foam effects
from the data and found that the roughness effect was somewhat less than the Stogryn theory
would predict by a frequency dependent factor. Using airborne data, Nordberg et al. 
characterized the combined foam and roughness effect at 19.35 GHz. At their measurement
angle the observed effect was dominated by foam. Stogryn’s geometric optics theory was
extended to included diffraction effects, multiple scattering, and two-scale partitioning by
Wu and Fung  and Wentz .
The first simultaneous retrieval of W, V, and L was based on airborne data from the
1973 joint US-USSR Bering Sea Experiment (BESEX) [Wilheit and Fowler, 1977]. Later
Chang and Wilheit  combined two NIMBUS-5 instruments, the ESMR and the NEMS
for a W, V, and L retrieval. Wilheit [1979a] used the 37-GHz dual polarized data from the
Electrically Scanned Microwave Radiomter (ESMR) to explore the wind-induced roughness
of the ocean surface. This was later combined with other data to generate a semi-empirical
model for the ocean surface emissivity [Wilheit, 1979b] in preparation for the 1978 launch of
the Scanning Multichannel Microwave Radiometer (SMMR) on the Nimbus-7 and SeaSat
satellites. A theory for the retrieval of all 4 ocean parameters was published by Wilheit and
The launch of the SeaSat and Nimbus-7 SMMR’s spurred many investigation on SMMR
retrieval algorithms and model functions [Wentz, 1983; Njoku and Swanson, 1983; Al-
ishouse, 1983; Chang et al, 1984; Gloersen et al., 1984], and the state-of-the-art in oceanic
microwave radiometry quickly advanced. It became clear that the water vapor retrievals
were highly accurate. A major improvement in the wind retrieval was made when Wentz et
al.  combined the SeaSat SMMR TB’s and the SeaSat scatterometer (SASS) wind re-
trievals to develop an accurate, semi-empirical relationship for the wind-induced emissivity.
Sea-surface temperature retrievals have been less successful. The measurement of TS re-
quires relatively low microwave frequencies (4-10 GHz). The SMMR’s were the first satel-
lite sensors with the appropriate frequencies to retrieve TS. However, the SMMR’s suffered
from a poor calibration design, and the reported T S retrievals [Njoku and Swanson, 1983;
Milman and Wilheit, 1985] were useful for little more than a demonstration of the possibility
of TS retrievals for future, better calibrated radiometers.
The next major milestone was the launch of the Special Sensor Microwave Imager
(SSM/I) in 1987. In contrast to SMMR, SSM/I has an external calibration system that pro-
vides stable observations. Unfortunately, the lowest SSM/I frequency is 19.3 GHz, and
hence TS retrievals are not possible. Shortly after the launch, there was a flurry of new SSM/
I algorithms. Most of these algorithms, such as the Goodberlet et al.  wind algorithm
and the Alishouse et al.  vapor algorithm, were simply statistical regressions to in situ
data (see Section 3.5). These algorithms performed reasonably well but provided no infor-
mation on the relevant physics. A more physical approach to algorithm development for
SSM/I was taken by Schluessel and Luthardt  and Wentz [1992, 1997]. This physical
approach to algorithm development is described herein and will be the basis for the AMSR
In November 1997, the first microwave radiometer capable of accurately measuring SST
through clouds was launched on the Tropical Rainfall Measuring Mission (TRMM) space-
craft. The TRMM Microwave Imager (TMI) is providing an unprecedented view of the
oceans. Its lowest frequency channel (10.7 GHz) penetrates non-raining clouds with little at-
tenuation, giving a clear view of the sea surface under all weather conditions except rain.
Furthermore at this frequency, atmospheric aerosols have no effect, making it possible to
produce a very reliable SST time series for climate studies. The one disadvantage of the mi-
crowave SST is spatial resolution. The radiation wavelength at 10.7 GHz is about 3 cm, and
at these long wavelengths the spatial resolution on the Earth surface for a single TMI obser-
vation is about 50 km. Also, the TRMM orbit was selected for continuous monitoring of the
tropics. To achieve this, a low inclination angle was chosen, confining the TRMM observa-
tions between 40°S and 40°N. Previous microwave radiometers were either too poorly cali-
brated or operated at too high of a frequency to provide a reliable estimate of SST. The early
results for the TMI SST retrievals are quite impressive and are already leading to improved
analyses in a number of important scientific areas, including tropical instability waves
(TIWs) and tropical storms [Wentz et al., 1999]
1.7. AMSR Instrument Characteristics
The PM AMSR instrument is similar to SSM/I. The major differences are that AMSR
has more channels and a larger parabolic reflector. AMSR takes dual polarization observa-
tions (v-pol and h-pol) at the 6 frequencies shown in Table 3. The offset 1.6-m diameter
parabolic reflector focuses the Earth radiation into an array of 6 feedhorns. The radiation
collected by the feedhorns is then amplified by 14 separate total-power radiometers. The
18.7 and 23.8 GHz receivers share a feedhorn, while dedicated feedhorns are provided for
the other frequencies. Two feedhorns are required for the 89 GHz channels to achieve a 5-
km along-track spacing. Figure 2 shows the block diagram for this configuration.
The parabolic reflector and feedhorn array are mounted on a drum containing the ra-
diometers, digital data subsystem, mechanical scanning subsystem, and power subsystem.
The reflector/feed/drum assembly is rotated about the axis of the drum by a coaxially mount-
ed bearing and power transfer assembly. All data, commands, timing and telemetry signals,
and power pass through the assembly on slip ring connectors to the rotating assembly.
A cold reflector and a warm load are mounted on the transfer assembly shaft and do not
rotate with the drum assembly. They are positioned off axis such that they pass between the
feedhorn array and the parabolic reflector, occulting it once each scan. The cold reflector re-
flects cold sky radiation into the feedhorn array thus serving, along with the warm load, as
calibration references for the AMSR.
The AMSR rotates continuously about an axis parallel to the spacecraft nadir at 40 rpm.
At an altitude of 705 km, it measures the upwelling Earth brightness temperatures over an
angular sector of ± 61° degrees about the sub-satellite track, resulting in a swath width of
1445 km. During a scan period of 1.5 seconds, the spacecraft sub-satellite point travels 10
km. Even though the instantaneous field-of-view for each channel is different, Earth obser-
vations are recorded at equal intervals of 10 km (5 km for the 89 GHz channels) along the
scan. The two 89-GHz feedhorns are offset such that their two scan lines are separated by 5
km in the along-track direction. The nadir angle for the parabolic reflector is fixed at 47.4°,
which results in an Earth incidence angle θi of 55° ± 0.3°. The small variation in θi is due to
the slight eccentricity of the orbit and the oblateness of the Earth.
As compared to the PM AMSR. the AMSR to fly on the ADEOS-2 spacecraft has two
additional frequencies: 50.3 and 52.8 GHz. The tables in Section 2 for the radiative transfer
model include these two additional frequencies.
Table 3. Instrument Specifications for PM AMSR
Center Frequencies (GHz) 6.925 10.65 18.7 23.8 36.5 89.0
Bandwidth (MHz) 350 100 200 400 1000 3000
Sensitivity (K) 0.3 0.6 0.6 0.6 0.6 1.1
IFOV (km x km) 76 × 44 49× 28 28 × 16 31 × 18 14 × 8 6×4
Sampling Rate (km x km) 10 × 10 10 × 10 10× 10 10 × 10 10 × 10 5×5
Integration Time (msec) 2.6 2.6 2.6 2.6 2.6 1.3
Main Beam Efficiency (%) 95.3 95.0 96.3 96.4 95.3 96.0
Beamwidth (degrees) 2.2 1.4 0.8 0.9 0.4 0.18
6.9 GHz V-Pol Square-Law
6.9 V counts
6.9 GHz H-Pol Square-Law 6.9 H counts
10.7 GHz V-Pol Square-Law
10.7 V counts
10.7 GHz H-Pol Square-Law 10.7 H counts
18.7 GHz V-Pol Square-Law
18.7 V counts
23.8 GHz V-Pol Square-Law
Receiver Detector 23.8 V counts
18.7 GHz H-Pol Square-Law 18.7 H counts
23.8 GHz H-Pol Square-Law 23.8 H counts
36.5 GHz V-Pol Square-Law
Receiver Detector 36.5 V counts
36.5 GHz H-Pol Square-Law 36.5 H counts
89.0 GHz V-Pol Square-Law 89.0 V counts, A-scan
89.0 GHz H-Pol Square-Law
Receiver Detector 89.0 H counts, A-scan
89.0 GHz V-Pol Square-Law
Receiver Detector 89.0 V counts, B-scan
89.0 GHz H-Pol Square-Law
89.0 H counts, B-scan
Fig. 2. Block diagram for PM AMSR feedhorns and radiometers.
2. Geophysical Model for the Ocean and Atmosphere
The key component of the ocean parameter retrieval algorithm is the geophysical model
for the ocean and atmosphere. It is this model that relates the observed brightness tempera-
ture (TB) to the relevant geophysical parameters. In remote sensing, the specification of the
geophysical model is sometimes referred to as the forward problem in contrast to the inverse
problem of inverting the model to retrieve parameters. An accurate specification of the geo-
physical model is the crucial first step in developing the retrieval algorithm.
2.2. Radiative Transfer Equation
We begin by deriving the radiative transfer model for the atmosphere bounded on the
bottom by the Earth’s surface and on the top by cold space. The derivation is greatly simpli-
fied by using the absorption-emission approximation in which radiative scattering from large
rain drops and ice particles is not included. Over the spectral range from 6 to 37 GHz, the
absorption-emission approximation is valid for clear and cloudy skies and for light rain up to
about 2 mm/h. The results of Wentz and Spencer  indicate that only 3% of the SSM/I
observations over the oceans viewed rain rates exceeding 2 mm/h. Thus, the absorption-
emission model to be presented will be applicable to about 97% of the AMSR ocean obser-
In the microwave region, the radiative transfer equation is generally given in terms of the
radiation brightness temperature (TB), rather than radiation intensity. So we first give a brief
discussion on the relationship between radiation intensity and T B. Let Pλ denote the power
within the wavelength range dλ, coming from a surface area dA, and propagating into the
solid angle dΩ. The specific intensity of radiation Iλ is then defined by
P = I λ cos θi dλ dA dΩ
The specific intensity is in units of erg/s-cm3-steradian. The angle θi is the incidence angle
defined as the angle between the surface normal and the propagation direction. For a black
body, Iλ is given by Planck’s law to be [Reif, 1965]
2 hc 2
λ5 exp hc λkT − 1f (2)
where c is the speed of light (2.998×1010 cm/s), h is Planck’s constant (6.626×10−27 erg-s), k
is Boltzmann’s constant (1.381×10−16 erg/K), λ (cm) is the radiation wavelength, and T (K)
is the temperature of the black body. Consider a surface that is emitting radiation with a spe-
cific intensity Iλ. Then the brightness temperature TB for this surface is defined as the tem-
perature at which a black body would emit the radiation having specific intensity Iλ. In the
microwave region, the exponent in (2) is small compared to unity, and (2) can be easily in-
verted to give TB in terms of Iν.
λ4 I λ
TB = (3)
This approximation is the well known Rayleigh Jeans approximation for λ >> hc/kT.
In terms of TB, the differential equation governing the radiative transfer through the at-
= −α(s) TB (s) − T(s) (4)
where the variable s is the distance along some specified path through the atmosphere. The
terms α(s) and T(s) are the absorption coefficient and the atmospheric temperature at posi-
tion s. Equation (4) is simply stating that the change in T B is due to (1) the absorption of ra-
diation arriving at s and (2) to emission of radiation emanating from s. We let s = 0 denote
the Earth’s surface, and let s = S denote the top of the atmosphere (i.e., the elevation above
which α(s) is essentially zero).
Two boundary conditions that correspond to the Earth’s surface at the bottom and cold
space at the top are applied to equation (4). The surface boundary conditions states that the
upwelling brightness temperature at the surface TB↑ is the sum of the direct surface emission
and the downwelling radiation that is scattered upward by the rough surface [Peake, 1959].
z z b g b g
sec θ i
TBAk i ,0) = E(k i )TS +
( sin θs dθs dϕ s TBBks ,0) σ o,c k s , k i + σ o, × k s , ki
4π 0 0
where the first TB argument denotes the propagation direction of the radiation and the second
argument denotes the path length s. The unit propagation vectors ki and ks denote the direc-
tion of the upwelling and downwelling radiation, respectively. In terms of polar angles in a
coordinate system having the z-axis normal to the Earth’s surface, these propagation vectors
are given by
ki = cos ϕ i sin θi ,sin ϕ i sin θi ,cos θi (6a)
k s = − cos ϕ s sin θs ,sin ϕ s sin θs , cos θs (6b)
The first term in (5) is the emission from the surface, which is the product of the surface
temperature TS and the surface emissivity E(ki). The second term is the integral of down-
welling radiation TB↓(ks) that is scattered in direction ki. The integral is over the 2π steradian
of the upper hemisphere. The rough surface scattering is characterized by the bistatic nor-
malized radar cross sections (NRCS) σo,c(θs,θi) and σo,×(θs,θi). These cross sections specify
what fraction of power coming from ks is scattered into ki. The subscripts c and × denote co-
polarization (i.e., incoming and outgoing polarization are the same) and cross-polarization
(i.e., incoming and outgoing polarizations are orthogonal), respectively. The cross sections
also determine the surface reflectivity R(ki) via the following integral.
z z b g b g
R( k i ) = sin θs dθs dϕ s σ o,c k s , ki + σ o, × k s , k i (7)
4π 0 0
The surface emissivity E(ki) is given by Kirchhoff’s law to be
E( k i ) = 1 − R( k i ) (8)
It is important to note that equations (5) an (7) provide the link between passive microwave
radiometry and active microwave scatterometry. The scatterometer measures the radar
backscatter coefficient, which is simply σo,c(-ki,ki).
The upper boundary condition for cold space is
TBBk s , S) = TC
This simply states that the radiation coming from cold space is isotropic and has a magnitude
of TC = 2.7 K.
The differential equation (4) is readily solved by integrating and applying the two bound-
ary conditions (5) and (9). The result for the upwelling brightness temperature at the top of
the atmosphere (i.e., the value observed by Earth-orbiting satellites) is
TBAk i , S) = TBU + τ ETS + TBΩ
where TBU is the contribution of the upwelling atmospheric emission, τ is the total transmit-
tance from the surface to the top of the atmosphere, E is the Earth surface emissivity given
by (8), and TBΩ is the surface scattering integral in (5). The atmospheric terms can be ex-
pressed in terms of the transmittance function τ(s1,s2)
b g Fz I
τ s1 , s2 = exp − ds α(s) (11)
which is the transmittance between points s1 and s2 along the propagation path ks or ki. The
total transmittance τ in (10) is given by
τ = τ 0,Saf (12)
and the upwelling and downwelling atmosphere emissions are given by
TBU = ds α(s) T(s) τ(s, S) (13a)
TBD = ds α(s) T(s) τ(0, s) (13b)
The sky radiation scattering integral is
z z b g b g
sec θ i
TBΩ = sin θs dθs dϕ s ( TBD + τTC ) σ o,c k s , k i + σ o, × k s , ki (14)
4π 0 0
Thus, given the temperature TS and absorption coefficient α at all points in the atmo-
sphere and given the surface bistatic cross sections, T B can be rigorously calculated. Howev-
er, in practice, the 3-dimensional specification of TS and α over the entire volume of the at-
mosphere is not feasible, and to simplify the problem, the assumption of horizontal uniformi-
ty is made. That is to say, the absorption is assumed to only be a function of the altitude h
above the Earth’s surface, i.e., α(s) = α(h). To change the integration variable from ds to
dh, we note that for the spherical Earth
∂s 1+ δ
∂h cos θ + δ(2 + δ )
where θ is either θi or θs, δ = h/RE, and RE is the radius of the Earth. In the troposphere δ <<
1, and an excellent approximation for θ < 60° is,
= sec θ (16)
With this approximation and the assumption of horizontal uniformity, the above equations
reduce to the following expressions.
Fsec dh I
τb , h , θg expG θ z α( h )J
h 1 2 = − (17)
τ = τb H, θ g
TBU = sec θi dh α( h ) T( h ) τ( h, H, θi ) (19a)
TBD = sec θs dh α( h ) T( h ) τ(0, h, θs ) (19b)
Thus, the brightness temperature computation now only requires the vertical profiles of T(h)
and α(h) along with the surface cross sections. The following two sections discuss the atmo-
spheric model for α(h) and the sea-surface model for the cross sections, respectively. In
closing, we note that the AMSR incidence angle is 55° and hence approximation (16) is quite
valid, with one exception. In the scattering integral, θs goes out to 90°, and in this case we
use (15) to evaluate the integral.
2.3. Model for the Atmosphere
In the microwave spectrum below 100 GHz, atmospheric absorption is due to three com-
ponents: oxygen, water vapor, and liquid water in the form of clouds and rain [Waters,
1976]. The sum of these three components gives the total absorption coefficient
α( h ) = α O ( h ) + α V ( h ) + α L ( h ) (20)
Numerous investigators have studied the dependence of the oxygen and water vapor coeffi-
cients on frequency ν (GHz), temperature T (K), pressure P (mb), and water vapor density
ρV (g/cm3) [Becker and Autler, 1946; Rozenkranz, 1975; Waters, 1976; Liebe, 1985]. To
specify αO and αV as a function of (ν,T,P,ρV) we use the Liebe  expressions with one
modification. The self-broadening component of the water vapor continuum is reduced by a
factor of 0.52 (see below). The liquid water coefficient αL comes directly from the Rayleigh
approximation to Mie scattering and is a function of T and the liquid water density ρL
(g/cm2) (see below). Figure 3 shows the total atmospheric absorption for each component.
Results for three water vapor cases (10, 30, and 60 mm) are shown. The cloud water content
is 0.2 mm. This corresponds to a moderately heavy non-raining cloud layer.
Let AI denote the vertically integrated absorption coefficient.
A I = dh α I ( h ) (21)
where h is the height (cm) above the Earth’s surface and subscript I equals O, V, or L. Equa-
tions (17) and (18) then give the total transmittance to be
τ = exp − sec θ i A O + A V + A L g (22)
Assuming for the moment that the atmospheric temperature is constant, i.e., T(h) = T, then
the integrals in equations (19) can be exactly evaluated in closed form to yield
TBU = TBD = 1 − τ T (23)
In reality, the atmospheric temperature does vary with h, typically decreasing at a lapse rate
of about -5.5 C/km in the lower to mid troposphere. In view of (23), we find it convenient to
parameterize the atmospheric model in terms of the following upwelling and downwelling
effective air temperatures:
TU = TBU / (1 − τ) (24a)
TD = TBD / (1 − τ) (24b)
These effective temperatures are indicative of the air temperature averaged over the lower to
mid troposphere. Note that in the absence of significant rain, TU and TD are very similar in
value, with TU being 1 to 2 K colder.
In view of the above equations, one sees that the atmospheric model can be parameter-
ized in terms of the following 5 parameters:
1. Upwelling effective temperature TU
2. Downwelling effective temperature TD
3. Vertically integrated oxygen absorption AO
4. Vertically integrated water vapor absorption AV
5. Vertically integrated liquid water absorption AL
To study the properties of the first four parameters, we use a large set of 42,195 radiosonde
flights launched from small islands [Wentz, 1997]. These radiosonde reports provide air
temperature T(h), air pressure p(h), and water vapor density ρV(h) at a number of levels in
the troposphere. From these data, the coefficients αO and αV are computed from the Liebe
 expressions, except that the water vapor continuum term is modified as discussed in
the next paragraph. Performing the numerical integrations as indicated above, T U, TD, AO,
and AV are found for each radiosonde flight. In addition, the vertically integrated water va-
por V is also computed.
Total Atmosphere Attenuation (naper)
Water Vapor, 10 mm
Water Vapor, 30 mm
0.001 Water Vapor, 60 mm
Cloud, 0.20 mm
0 10 20 30 40 50 60 70 80 90 100
Fig. 3. The atmospheric absorption spectrum for oxygen, water vapor, and cloud water.
Results for three water vapor cases (10, 30, and 60 mm) are shown. The cloud water
content is 0.2 mm which corresponds to a moderately heavy non-raining cloud layer.
V = 10 dh ρV ( h ) (25)
where ρV(h) is in units of g/cm3, and the leading factor of 10 converts from g/cm2 to mm.
Wentz  computed AV directly from collocated SSM/I and radiosonde observations.
At 19, 22, and 37 GHz, the Liebe AV was found to be 4%, 3%, and 20% higher than the
SSM/I-derived value, respectively. To quote Liebe : ‘Water vapor continuum absorp-
tion has been a major source of uncertainty in predicting millimeter wave attenuation rates,
especially in the window ranges.’ The frequency of 37 GHz is in a water vapor window and
is most affected by the continuum. It should be noted that Liebe also needed to rely on com-
bined radiometer-radiosonde measurements to infer the continuum in the 6 to 37 GHz re-
gion. Liebe’s data set in this spectral region is rather limited and does not contain any 37
GHz observations. We believe the SSM/I method of deriving A V is more accurate than
Liebe’s method, and hence adjust the Liebe  water vapor spectrum so that it will agree
with the SSM/I results. We find that very good agreement is obtained by reducing the self-
broadening component of the water vapor continuum by a factor of 0.52. After this adjust-
ment, the agreement at all three frequencies is within ± 1%.
Figure 4 shows the TD values computed from the 42,195 radiosondes plotted versus V.
Three frequencies are shown (19, 22, and 37 GHz), and the curves are quite similar. The
solid lines in the figure show equation (26), and vertical bars show the ± one standard devia-
tion of TD derived from the radiosondes. For low to moderate values of V (0 to 40 mm), T D
increases with V, and above 40 mm, TD reaches a relatively constant value of 287 K. The T U
versus V curves (not shown) are very similar except that T U is 1 to 2 K colder. The follow-
ing least-square regressions are found to be a good approximation of the TD, TU versus V re-
TD = b 0 + b1V + b 2V 2 + b3V3 + b 4V 4 + b5 ς TS − TV g (26a)
TU = TD + b 6 + b 7 V (26b)
TV = 27316 + 0.8337 V − 3.029 × 10 −5 V3.33
. V ≤ 48 (27a)
TV = 30116
. V > 48 (27b)
b gF (T1200 ) I |T − T | ≤ 20K
G −T J
ς (TS − TV ) = 1.05 ⋅ TS − TV ⋅ 1 −
S V (27c)
ς (TS − TV ) = sign(TS − TV ) ⋅14K |TS − TV |> 20K (27d)
V is in units of millimeters and all temperatures are in units of Kelvin. When evaluating
(26a), the expression is linearly extrapolated when V is greater than 58 mm. We have in-
cluded a small additional term that is a function of the difference between the sea-surface
temperature TS and TV, which represents the sea-surface temperature that is typical for water
vapor V. The term ς ( TS − TV ) accounts for the fact that the effective air temperature is typi
Effective Air Temperature for Downwelling Radiation (K)
250 19 GHz
250 22 GHz
250 37 GHz
0 10 20 30 40 50 60 70
Columnar Water Vapor (mm)
Fig. 4. The effective air temperature TD for downwelling radiation plotted versus the
RAOB columnar water vapor. The solid curve is the model value, and the vertical bars
are the ± one standard deviation of TD derived from radiosondes.
cally higher (lower) for the case of unusually warm (cold) water. The TV versus V relation-
ship was obtained by regressing the climatology sea-surface temperature at the radiosonde
site to V derived from the radiosondes. Over the full range of V, the rms error in approxi-
mation (26) is typically about 3 K. Table 4 gives the b0 through b7 coefficients for all 8
Table 4. Model Coefficients for the Atmosphere
Freq. (GHz) 6.93E+0 10.65E+0 18.70E+0 23.80E+0 36.50E+0 50.30E+0 52.80E+0 89.00E+0
b0 (K) 239.50E+0 239.51E+0 240.24E+0 241.69E+0 239.45E+0 242.10E+0 245.87E+0 242.58E+0
b1 (K mm−1) 213.92E−2 225.19E−2 298.88E−2 310.32E−2 254.41E−2 229.17E−2 250.61E−2 302.33E−2
b2 (K mm−2) −460.60E− −446.86E− −725.93E− −814.29E− −512.84E− −508.05E− −627.89E− −749.76E−4
4 4 4 4 4 4 4
b3 (K mm−3) 457.11E−6 391.82E−6 814.50E−6 998.93E−6 452.02E−6 536.90E−6 759.62E−6 880.66E−6
b4 (K mm−4) −16.84E−7 −12.20E−7 −36.07E−7 −48.37E−7 −14.36E−7 −22.07E−7 −36.06E−7 −40.88E−7
b5 0.50E+0 0.54E+0 0.61E+0 0.20E+0 0.58E+0 0.52E+0 0.53E+0 0.62E+0
b6 (K) −0.11E+0 −0.12E+0 −0.16E+0 −0.20E+0 −0.57E+0 −4.59E+0 −12.52E+0 −0.57E+0
b7 (K mm−1) −0.21E−2 −0.34E−2 −1.69E−2 −5.21E−2 −2.38E−2 −8.78E−2 −23.26E−2 −8.07E−2
aO1 8.34E−3 9.08E−3 12.15E−3 15.75E−3 40.06E−3 353.72E−3 1131.76E−3 53.35E−3
aO2 (K ) −0.48E−4 −0.47E−4 −0.61E−4 −0.87E−4 −2.00E−4 −13.79E−4 −2.26E−4 −1.18E−4
aV1 (mm−1) 0.07E−3 0.18E−3 1.73E−3 5.14E−3 1.88E−3 2.91E−3 3.17E−3 8.78E−3
aV2 (mm ) 0.00E−5 0.00E−5 −0.05E−5 0.19E−5 0.09E−5 0.24E−5 0.27E−5 0.80E−5
Table 5. RMS Error in Oxygen and Water Vapor Absorption Approximation
Freq. (GHz) 6.93 10.65 18.70 23.80 36.50 50.30 52.80 89.00
Oxygen, AO 0.0002 0.0002 0.0003 0.0003 0.0008 0.0062 0.0163 0.0009
Vapor, AV 0.0001 0.0002 0.0011 0.0013 0.0025 0.0042 0.0046 0.0129
The vertically integrated oxygen absorption AO is nearly constant over the globe, with a
small dependence on the air temperature. We find the following expression to be a very
good approximation for AO:
A O = a O1 + a O 2 TD − 270 g (28)
Table 4 gives the aO coefficients for the 8 AMSR frequencies, and Table 5 gives the rms er-
ror in this approximation for the 8 frequencies. At 23.8 GHz and below, the error is negligi-
ble, being 0.0003 napers or less. At 36.5 GHz, the error is still quite small, being 0.0008
napers. Note that 0.001 napers roughly corresponds to a T B error of 0.5 K. For the 50.3 and
52.8 GHz oxygen band channels, the error is considerably larger, but (28) is not used for the
oxygen band channels. Rather the oxygen band channels can be used to retrieve TD.
The vapor absorption AV is primarily a linear function of V, although there is a small sec-
ond order term. We find the following expression is a good approximation for AV:
AV = aV1V + aV2V2 (29)
Table 4 gives the aV coefficients for the 8 AMSR frequencies, and Table 5 gives the rms er-
ror in this approximation for the 8 frequencies. For the 6.9 and 10.7 AMSR channels, the
rms error in this approximation is negligible, being 0.0002 napers or less. In the 18.7 to
36.5 range, the error remains relatively small (0.001 to 0.0025 napers), but not negligible.
The final atmospheric parameter to be specified is the vertically integrated liquid water
absorption AL. When the liquid water drop radius is small relative to the radiation wave-
length, the absorption coefficient αL (cm−1) is given by the Rayleigh scattering approxima-
tion [Goldstein, 1951]:
6 πρL ( h ) F I
λρo H K
where λ is the radiation wavelength (cm), ρL(h) is the density (g/cm3) of cloud water in the
atmosphere given as a function of h, ρo is the density of water (ρo ≈ 1 g/cm3), and ε is the
complex dielectric constant of water. Note that the dielectric constant varies with tempera-
ture and hence is also a function of h. Substituting (30) into (21) gives
0.6 πL F I
2+εH K (31)
where L is the vertically integrated liquid water (mm) given by
L = 10 dh ρL ( h ) (32)
The leading factor of 10 converts from g/cm2 to mm. In deriving (31), we have assumed the
cloud is at a constant temperature. For the more realistic case of the temperature varying
with height, ε should be evaluated at some mean effective temperature for the cloud. The
specification of ε as a function of temperature and frequency is given in Section 2.4. An ex-
cellent approximation for (31) is found to be
A L = a L1 1 − a L 2 (TL − 283) L (33)
where TL is the mean temperature of the cloud, and the aL coefficients are given in Table 6
for the 8 AMSR frequencies. The error in this approximation is ≤ 1% over the range of TL
from 273 to 288 K, which is negligible compared to other errors such as the uncertainty in
specifying the cloud temperature TL. Note that in the retrieval algorithm, the error in speci-
fying TL only effects the retrieved value of L. The retrieval of the other parameters only re-
quires the spectral ratio of AL, which is essentially independent of T L due to the fact that aL2
is spectrally flat.
In the absence of rain, the cloud droplets are much smaller than the radiation wave-
lengths being considered, and equations (31) and (33) are valid. When rain is present, Mie
scattering theory must be used to compute AL. For light rain not exceeding 2 mm/h and for
frequencies between 6 and 37 GHz, the Mie scattering computations give the following ap-
proximation [Wentz and Spencer, 1998]:
Table 6. Coefficients for Rayleigh Absorption and Mie Scattering.
Freq (GHz) 6.93 10.65 18.70 23.80 36.50 50.30 52.80 89.00
aL1 0.0078 0.0183 0.0556 0.0891 0.2027 0.3682 0.4021 0.9693
aL2 0.0303 0.0298 0.0288 0.0281 0.0261 0.0236 0.0231 0.0146
aL3 0.0007 0.0027 0.0113 0.0188 0.0425 0.0731 0.0786 0.1506
aL4 0.0000 0.0060 0.0040 0.0020 -0.0020 -0.0020 -0.0020 -0.0020
aL5 1.2216 1.1795 1.0636 1.0220 0.9546 0.8983 0.8943 0.7961
A R = a L3 ⋅ 1 + a L4 ⋅ ( TL − 283) ⋅ H ⋅ R a L5 (34a)
The rain column height H (in km) can be approximated by:
H = 1+ 0.14 ⋅ (TS − 273) − 0.0025 ⋅ (TS − 273)2 if TS < 301 (34b)
H = 2.96 if TS ≥ 301, (34c)
where TS denotes the sea surface temperature (in K). The rain rate R (in mm/h) is related to
the liquid cloud water density L by
L = 0.18 ⋅ 1 + HR . i (34d)
In deriving (34a) we have used a Marshall and Palmer  drop size distribution.
2.4. Dielectric Constant of Sea-Water and the Specular Sea Surface
A key component of the sea-surface model is the dielectric constant ε of sea water. The
parameter is a complex number that depends on frequency ν, water temperature TS, and wa-
ter salinity s. The dielectric constant is given by [Debye,1929; Cole and Cole, 1941] as
εS − ε∞ 2 jσλ
ε = ε∞ + 1− η − (35)
1 + jλ R λ c
where j = −1 , λ (cm) is the radiation wavelength, εε is the dielectric constant at infinite
frequency, εS is the dielectric constant for zero frequency (i.e., the static dielectric constant),
and λR (cm) is the relaxation wavelength. The spread factor η is an empirical parameter that
describes the distribution of relaxation wavelengths. The last term accounts for the conduc-
tivity of salt water. In this term, σ (sec−1, Gaussian units) is the ionic conductivity and c is
the speed of light.
Several investigators have developed models for the dielectric constant of sea water. In
the Stogryn  model the salinity dependence of εS and λR was based on the Lane and
Saxton  laboratory measurements of saline solutions. Stogryn noted that the Lane-
Saxton measurements for distilled water did not agree with those of other investigators. The
Klein and Swift  model is very similar to Stogryn model except that the salinity depen-
dence of εS was based on more recent 1.4 GHz measurements [Ho and Hall, 1973; Ho et al.,
1974]. Klein-Swift noted that their εS was significantly different from that derived from the
Lane and Saxton measurements. It appears that there may be a problem with Lane-Saxton
measurements. However, in the Klein-Swift model, the salinity dependence of λR was still
based on the Lane-Saxton measurements. We analyzed all the measurements used by
Stogryn and Klein-Swift and concluded that the Lane-Saxton measurements of ε for both
distilled water and salt water were inconsistent with the results reported by all other investi-
gators. Therefore, we completely exclude the Lane-Saxton measurements from our model
The model to be presented is very similar to the Klein-Swift model, with two exceptions.
First, since we excluded Lane-Saxton measurements, the salinity dependence of λR is differ-
ent. For cold water (0 to 10 C), our λR is about 5% lower than the Klein-Swift value and for
warm water (30 C), it is about 1% higher. Second, our value for εε is 4.44 and the Klein-
Swift value is 4.9, which was the value used by Stogryn. In the Stogryn model, η = 0,
whereas in the Klein-Swift model, η = 0.02. Grant et al.  pointed out that the choice
of εε depends on the choice for η, where η = 0 → εε = 4.9 and η = 0.02 → εε = 4.5. Thus
the Klein-Swift value of εε = 4.9 is probably too high. In terms of brightness temperatures,
these λR and εε differences are most significant at the higher frequencies. For example, at 37
GHz and θi = 55°, the difference in specular brightness temperatures produced by our model
and the Klein-Swift model differ by about ± 2 K. Analyses of SSM/I observations show that
our new model, as compared to the Klein-Swift model, produces more consistent retrievals
of ocean parameters. For example, using the Klein-Swift model resulted in an abundance of
negative cloud water retrievals in cold water. This problem no longer occurs with the new
model. (The negative cloud water problem was the original motivation for doing this reanal-
ysis of the ε model.)
We first describe the dielectric constant model for distilled water, and then extend the
model to the more general case of a saline solution. The static dielectric constant εS0 for dis-
tilled water has been measured by many investigators. The more recent measurements
[Malmberg and Maryott, 1956; Archer and Wang, 1990] are in very good agreement (0.2%).
The Archer and Wang  values for εS0, which are reported in the Handbook of Chem-
istry and Physics [Lide,1993], are regressed to the following expression:
ε S0 = 87.90 exp( −0.004585 t S ) (36)
where tS is the water temperature in Celsius units. The accuracy of the regression relative to
the point values for εS0 is 0.01% over the range from 0 to 40 C.
The other three parameters for the dielectric constant of distilled water are the relaxation
wavelength λR0, the spread factor η, and εε . We determine these parameters by a least-
squares fit of (35) to laboratory measurements εmea of the dielectric constant for the range
from 1 to 40 GHz. A literature search yielded ten papers reporting εmea for distilled water.
Values for λR0, η, and εε are found so as to minimize the following quantity:
Q = Re(ε − ε mea ) + Im(ε − ε mea )
The relaxation wavelength is a function of temperature [Grant et al., 1957], but it is general-
ly assumed that η and εε are independent of temperature. The least squares fit yields η =
0.012, εε = 4.44, and
λ R 0 = 3.30 exp( −0.0346 t S + 0.00017 t S )
These values are in good agreement with those obtained by other investigators. Our λR0
agrees with the expression derived by Stogryn  to within 1%. The values for η (εε ) re-
ported in the literature vary from 0 to 0.02 (4 to 5). Note that using a larger value for η ne-
cessitates using a smaller value for εε .
The presence of salt in the water produces ionic conductivity σ and modifies εS and λR.
It is generally assumed that η and εε are not affected by salinity. Weyl  found the fol-
lowing regression for the conductivity of sea water.
σ = 3.39 × 10 9 C 0.892 exp − ∆ tζ (39)
ζ = 2.03 × 10 −2 + 1.27 × 10 −4 ∆ t + 2.46 × 10 −6 ∆2t − C 3.34 × 10 −5 − 4.60 × 10 −7 ∆ t + 4.60 × 10 −8 ∆2t (40)
C = 0.5536 s (41)
∆ t = 25 − t S (42)
where s and C are salinity and chlorinity in units of parts/thousand. Note that we have con-
verted the Weyl conductivity to Gaussian units of sec−1.
To determine the effect of salinity on εS, we use low frequency (1.43 and 2.65 GHz)
measurements of ε for sea water and saline solutions [Ho and Hall, 1973; Ho et al., 1974].
For the Ho-Hall data, only the real part of the dielectric constant is used in the fit. Klein and
Swift reported that the measurements of the imaginary part were in error. To determine the
effect of salinity on λR, we use higher frequency (3 to 24 GHz) measurements of ε for saline
solutions [Haggis et al., 1952; Hasted and Sabeh, 1953; Hasted and Roderick, 1958]. A
least-squares fit to these data shows that the salinity dependence of εS and λR can be modeled
ε S = ε S0 exp −3.45 × 10 −3 s + 4.69 × 10 −6 s2 + 1.36 × 10 −5 st S h (43)
λ R = λ R 0 − 6.54 × 10 −3 1 − 3.06 × 10 −2 t S + 2.0 × 10 −4 t S s
The accuracy of the dielectric constant model is characterized in terms of its correspond-
ing specular brightness temperature TB. For each laboratory measurement of ε, we compute
the specular TB for an incidence angle of 55° using the Fresnel equation (45) below. Two
TB’s are computed: one using εmea and the other using the model ε coming from the above
equations. For the low frequency Ho-Hall data, the rms difference between the ‘measure-
ment’ TB and the ‘model’ TB is about 0.1 K for v-pol and 0.2 K for h-pol. For the higher fre-
quency data set, the rms difference is 0.8 K for v-pol and 0.5 K for h-pol.
Once the dielectric constant is known, the v-pol and h-pol reflectivity coefficients ρV and
ρH for a specular (i.e., perfectly flat) sea surface are calculated from the well-known Fresnel
ε cos θi − ε − sin 2 θi
ρv = (45a)
ε cos θi + ε − sin 2 θi
cos θi − ε − sin 2 θ i
ρh = (45b)
cos θ i + ε − sin 2 θi
where θI is the incidence angle. The power reflectivity R is then given by
R 0 p = ρp (46)
where subscript 0 denotes that this is the specular reflectivity and subscript p denotes polar-
An analysis using TMI data indicates small deviations from the model function for the di-
electric constant of sea water as discussed above. The effect is mainly noted in the v-pol re-
flectivity. In order to account for these small differences a correction term of
0v b g
= 4.887 ⋅ 10−8 − 6108 ⋅10−8 ⋅ TS − 273
is added to the v-pol reflectivity R 0v in (46). The resulting changes in the brightness temper-
ature range from about +0.14K in cold water to about –0.36K in warm water.
2.5. The Wind-Roughened Sea Surface
It is well known that the microwave emission from the ocean depends on surface rough-
ness. A calm sea surface is characterized by a highly polarized emission. When the surface
becomes rough, the emission increases and becomes less polarized (except at incidence an-
gles above 55º for which the vertically polarized emission decreases). There are three mech-
anisms that are responsible for this variation in the emissivity. First, surface waves with
wavelengths that are long compared to the radiation wavelength mix the horizontal and verti-
cal polarization states and change the local incidence angle. This phenomenon can be mod-
eled as a collection of tilted facets, each acting as an independent specular surface [Stogryn,
1967]. The second mechanism is sea foam. This mixture of air and water increases the
emissivity for both polarizations. Sea foam models have been developed by Stogryn 
and Smith . The third roughness effect is the diffraction of microwaves by surface
waves that are small compared to the radiation wavelength. Rice  provided the basic
formulation for computing the scattering from a slightly rough surface. Wu and Fung 
and Wentz  applied this scattering formulation to the problem of computing the emis-
sivity of a wind-roughened sea surface.
These three effects can be parameterized in terms of the rms slope of the large-scale
roughness, the fractional foam coverage, and the rms height of the small-scale waves. Each
of these parameters depends on wind speed. Cox and Munk , Monahan and O'Muirc-
heartaigh , and Mitsuyasu and Honda  derived wind speed relationships for the
three parameters, respectively. These wind speed relationships in conjunction with the
tilt+foam+diffraction model provide the means to compute the sea-surface emissivity. Com-
putations of this type have been done by Wentz [1975, 1983] and are in general agreement
with microwave observations.
In addition to depending on wind speed, the large-scale rms slope and the small-scale
rms height depend on wind direction. The probability density function of the sea-surface
slope is skewed in the alongwind axis and has a larger alongwind variance than crosswind
variance [Cox and Munk, 1954]. The rms height of capillary waves is very anisotropic [Mit-
suyasu and Honda, 1982]. The capillary waves traveling in the alongwind direction have a
greater amplitude than those traveling in the crosswind direction. Another type of direction-
al dependence occurs because the foam and capillary waves are not uniformly distributed
over the underlying structure of large-scale waves. Smith's  aircraft radiometer mea-
surements show that the forward plunging side of a breaking wave exhibits distinctly warmer
microwave emissions than does the back side. In addition, the capillary waves tend to clus-
ter on the downwind side of the larger gravity waves [Cox, 1958; Keller and Wright, 1975].
The dependence of foam and capillary waves on the underlying structure produces an up-
wind-downwind asymmetry in the sea-surface emissivity.
The anisotropy of capillary waves is responsible for the observed dependence of radar
backscattering on wind direction [Jones et al., 1977]. The upwind radar return is consider-
ably higher than the crosswind return. Also, the modulation of the capillary waves by the
underlying gravity waves causes the upwind return to be generally higher than the downwind
return. These directional characteristics of the radar return have provided the means to sense
wind direction from aircraft and satellite scatterometers [Jones et al., 1979].
To model the rough sea surface, we begin by assuming the surface can be partitioned into
foam-free areas and foam-covered areas within the radiometer footprint. The fraction of the
total area that is covered by foam is denoted by f. The composite reflectivity is then given
R = (1 − f )R clear + fκR clear (47)
where Rclear is the reflectivity of the rough sea surface clear of foam, and the factor κ ac-
counts for the way in which foam modifies the reflectivity. As discussed above, foam tends
to decrease the reflectivity, and hence κ < 1. The reflectivity of the clear, rough sea surface
is modeled by the following equation:
R clear = (1 − β) R geo (48)
where Rgeo is the reflectivity given by the standard geometric optics model (see below) and
the factor 1 − β accounts for the way in which diffraction modifies the geometric-optics re-
flectivity. Wentz  showed that the inclusion of diffraction effects is a relatively small
effect and hence β small compared to unity.
Combining the above two equations gives
R = (1 − F )R geo (49)
F = f + β − fβ − fκ + fκβ (50)
where F is a ‘catch-all’ term that accounts for both foam and diffraction effects. All of the
terms that makeup F are small compared to unity, and the results to be presented show that F
< 10%. The reason we lump foam and diffraction effects together is that they both are diffi-
cult to model theoretically. Hence, rather than trying to compute F theoretically, we let F be
a model parameter that is derived empirically from various radiometer experiments. Howev-
er, the Rgeo term is theoretically computed from the geometric optics. Thus, the F term is a
measure of that portion of the wind-induced reflectivity that is not explained by the geomet-
The geometric optics model assumes the surface is represented by a collection of tilted
facets, each acting as an independent reflector. The distribution of facets is statistically char-
acterized in terms of the probability density function P(S u,Sc) for the slope of the facets,
where Su and Sc are the upwind and crosswind slopes respectively. Given this model, the re-
flectivity can be computed from equation (7). To do this, the integration variables θs,φs in
(7) are transformed to the surface slope variables. The two equations governing this trans-
k s = k i − 2 ki ⋅ n n (51)
− Su , − Sc , 1
1 + S2 + S2
where n is the unit normal vector for a given facet. Transforming (7) to the S u,Sc integration
b g g b g
z z P(S ,S ) 1 + S + S b ⋅ ng
dSu dSc P(Su , Sc ) 1 + S2 + S2 k i ⋅ n p ⋅ hi ρh hs + p ⋅ v i ρv v s χ(k s )(1 − R × ) + R ×
R geo =
u c u kc u c i
where p is the unit vector specifying the reflectivity polarization. The unit vectors hi and vi
(hs and vs) are the horizontal and vertical polarization vectors associated with the propagation
vector ki (ks) as measured in the tilted facet reference frame. These polarization vectors in
the tilted frame of reference are given by
hj = j (54a)
kj × n
vj = kj × hj (54b)
where subscript j = i or s. The terms ρv and ρh are the v-pol and h-pol Fresnel reflection co-
efficients given above. The last factor in (53) accounts for multiple reflection (i.e., radiation
reflecting off of one facet and then intersecting another). χ(ks) is the shadowing function
given by Wentz , and R× is the reflectivity of the secondary intersection. The shadow-
ing function χ(ks) essentially equals unity except when ks approaches surface grazing angles.
The interpretation of (53) is straightforward. The integration is over the ensemble of tilt-
ed facets having a slope probability of P(Su,Sc). The term 1 + Su + Sc k i ⋅ n is proportional
to the solid angle subtended by the tilted facet as seen from the observation direction speci-
b g b g 2
fied by ki. The term p ⋅ hi ρh h s + p ⋅ v i ρv v s is the reflectivity of the tilted facet. And, the
denominator in (53) properly normalizes the integral.
To specify the slope probability we use a Gaussian distribution as suggested by Cox and
Munk , and we assume that the upwind and crosswind slope variances are the same.
Wind direction effects are considered in Section 2.7. Then, the slope probability is given by
LS − S O
P(S , S ) = c S hexp M
− 2 −1
u c 2
where ∆S2 is the total slope variance defined as the sum of the upwind and crosswind slope
variances. Ocean waves with wavelengths shorter than the radiation wavelength do not con-
tribute to the tilting of facets and hence should not be included in the ensemble specified by
P(Su,Sc). For this reason, the effective slope variance ∆S2 increases with frequency, reaching
a maximum value referred to as the optical limit. The results of Wilheit and Chang 
and Wentz  indicate that the optical limit is reached near ν = 37 GHz. Hence, for ν ≥
37 GHz, we use the Cox and Munk  expression for optical slope variance. For lower
frequencies, a reduction factor is applied to the Cox and Munk expression. This reduction
factor is based on ∆S2 values derived from the SeaSat SMMR observations [Wentz, 1983].
∆S2 = 5.22 × 10 −3 W ν ≥ 37 GHz (56a)
∆S2 = 5.22 × 10 −3 1 − 0.00748(37 − ν)1.3 W ν < 37 GHz (56b)
where W is the wind speed (m/s) measured 10 m above the surface. Note the Cox and Munk
wind speed was measured at a 12.5 m elevation. Hence, their coefficient of 5.12×10−3 is in-
creased by 2% to account for our wind being referenced to a 10 m elevation.
The sea-surface reflectivity Rgeo is computed for a range of winds varying from 0 to 20
m/s, for a range of sea-surface temperatures varying from 273 to 303 K, and for a range of
incidence angles varying from 49° to 57°. These computations require the numerical evalua-
tion of the integral in equation (53). The integration is done over the range S2 + S2 ≤ 4.5∆S2 .
Facets with slopes exceeding this range contribute little to the integral, and it is not clear if a
Gaussian slope distribution is even applicable for such large slopes. Analysis shows that the
computed ensemble of Rgeo is well approximated by the following regression:
b gb gb g
R geo = R 0 − r0 + r1 θi − 53 + r2 TS − 288 + r3 θi − 53 TS − 288 W g (57)
where the first term R0 is the specular power reflectivity given by (46) and the second term is
the wind-induced component of the sea-surface reflectivity. The r coefficients are given in
Table 7 for all AMSR channels. Equation (57) is valid over the incidence angle from 49° to
57°. It approximates the θi and TS variation of Rgeo with an equivalent accuracy of 0.1 K.
The approximation error in the wind dependence is larger. In the geometric optics computa-
tions, the variation of Rgeo with wind is not exactly linear. In terms of T B, the non-linear
component of Rgeo is about 0.1 K at the lower frequencies and 0.5 K at the higher frequen-
cies. However, in view of the general uncertainty in the geometric optics model, we will use
the simple linear expression for Rgeo, and let the empirical F term account for any residual
non-linear wind variations, as is discussed in the next paragraph.
In the case of the coefficients r2 we do not use the geometric optics model coefficients (Ta-
ble 7) but rather use the following empirically derived forms (units are s/m-K):
bg = −21⋅10
bg = −5.5 ⋅10
+ 0.989 ⋅10−6 ⋅ 37 − ν if ν ≤ 37 (59a)
bg = −5.5 ⋅10
if ν > 37. (59b)
This accounts for the observations that the wind induced emissivity is less in warm water.
This effect was observed during the monsoons in the Arabian sea.
Table 7. Model Coefficients for Geometric Optics
Freq. (GHz) 6.93E+0 10.65E+0 18.70E+0 23.80E+0 36.50E+0 50.30E+0 52.80E+0 89.00E+0
v-pol r0 −0.27E−03 −0.32E−03 −0.49E−03 −0.63E−03 −1.01E−03 −1.20E−03 −1.23E−03 −1.53E−03
h-pol r0 0.54E−03 0.72E−03 1.13E−03 1.39E−03 1.91E−03 1.97E−03 1.97E−03 2.02E−03
v-pol r1 −0.21E−04 −0.29E−04 −0.53E−04 −0.70E−04 −1.05E−04 −1.12E−04 −1.13E−04 −1.16E−04
h-pol r1 0.32E−04 0.44E−04 0.70E−04 0.85E−04 1.12E−04 1.18E−04 1.19E−04 1.30E−04
v-pol r2 0.01E−05 0.11E−05 0.48E−05 0.75E−05 1.27E−05 1.39E−05 1.40E−05 1.15E−05
h-pol r2 0.00E−05 −0.03E−05 −0.15E−05 −0.23E−05 −0.36E−05 −0.32E−05 −0.30E−05 0.00E−05
v-pol r3 0.00E−06 0.08E−06 0.31E−06 0.41E−06 0.45E−06 0.35E−06 0.32E−06 −0.09E−06
h-pol r3 0.00E−06 −0.02E−06 −0.12E−06 −0.20E−06 −0.36E−06 −0.43E−06 −0.44E−06 −0.46E−06
r0 in units of s/m, r1 in units of s/m-deg, r2 in units of s/m-K, r3 in units of s/m-deg-K
In the 10-37 GHz band, the F term is found from collocated SSM/I-buoy and TMI-buoy
observations. The procedure for finding F is essentially the same as described by Wentz
 for finding the wind-induced emissivity, but in this case we first remove the geomet-
ric optics contribution to R. The F term is found to be a monotonic function of wind speed
F = m1 W W < W1 (60a)
F = m1W + 1 ( m 2 − m1 )( W − W1 )2 ( W2 − W1 )
2 W1 ≤ W ≤ W2 (60b)
F = m 2 W − 1 ( m 2 − m1 )( W2 + W1 )
2 W > W2 (60c)
This equation represents two linear segments connected by a quadratic spline such that the
function and its first derivative are continuous. The spline points are W1 = 3 m s and
W2 = 12 m s for the v-pol and W1 = 7 m s and W2 = 12 m s for the h-pol , respectively. The
m coefficients are found so that the T B model matches the SSM/I observations in the and
TMI observations when the buoy wind is used to specify W. For the lowest channel
ν = 6.9 GHz no data exist yet and we have simply used the same values as for the
ν = 10.65 GHz channel. This will be updated as soon as AMSR data become available. Table
8 summarizes the results for m1 and m 2 at the 8 AMSR frequencies for v and h polariza-
tions. Both coefficients flatten out and reach a maximum for ν ≥ 37 GHz.
Table 8. The coefficients m1 and m2. Units are s/m.
Freq. (GHz) 6.93 10.65 18.70 23.80 36.50 50.30 52.80 89.00
v-pol m1 0.00020 0.00020 0.00140 0.00178 0.00257 0.00260 0.00260 0.00260
h-pol m1 0.00200 0.00200 0.00293 0.00308 0.00329 0.00330 0.00330 0.00330
v-pol m2 0.00690 0.00690 0.00736 0.00730 0.00701 0.00700 0.00700 0.00700
h-pol m2 0.00600 0.00600 0.00656 0.00660 0.00660 0.00660 0.00660 0.00660
These results indicate that diffraction plays a significant role in modifying the sea-surface re-
flectivity. If diffraction were not important, β would be 0 in equation (50), and F would be pro-
portional to the fractional foam coverage f. Since f is essentially zero for W < 7 m/s, m1 would
be 0. This is not the case, and we interpret the m1 coefficient as an indicator of diffraction.
2.6. Atmospheric Radiation Scattered by the Sea Surface
The downwelling atmospheric radiation incident on the rough sea surface is scattered in
all directions. The scattering process is governed by the radar cross section coefficients σo as
indicated by equation (14). For a perfectly flat sea surface, the scattering process reduces to
simple specular reflection, for which radiation coming from the zenith angle θs is reflected
into zenith angle θi , where θs = θi. In this case, the reflected sky radiation is simply RTBD.
However, for a rough sea surface, the tilted surface facets reflect radiation for other parts of
the sky into the direction of zenith angle θi. Because the downwelling radiation TBD increas-
es as the secant of the zenith angle, the total radiation scattered from the sea surface is
greater than that given by simple specular reflection. The sea-surface reflectivity model dis-
cussed in the previous section is used to compute the scattered sky radiation TBΩ . These
computations show that TBΩ can be approximated by
TBΩ = [(1 + Ω)(1 − τ)( TD − TC ) + TC ] R (61)
where R is the sea-surface reflectivity given by (49), TBD is the downwelling brightness tem-
perature from zenith angle θi given by (24), and Ω is the fit parameter. The second term in
the brackets is the isotropic component of the cold space radiation. This constant factor can
be removed from the integral. The fit parameter for v-pol and h-pol is found to be
Ω V = [2.5 + 0.018(37 − ν) ][ ∆S2 − 70.0 ∆S6 ] τ3.4 (62a)
Ω H = [6.2 − 0.001(37 − ν)2 ][ ∆S2 − 70.0 ∆S6 ] τ 2.0 (62b)
where ν is frequency (GHz) and ∆S2 is the effective slope variance given by (56). The term
∆S2 − 70.0 ∆S6 reaches a maximum at ∆S2 = 0.069. For ∆S2 > 0.069, the term is held at its
maximum value of 0.046. ΩV has a linear dependence on frequency, whereas ΩH has a
quadratic dependence, reaching a maximum value at ν = 37 GHz. For ν > 37 GHz, both ΩV
and ΩH are held constant at their maximum values. Approximation (62) is valid for the
range of incidence angles from 52° to 56°. For moderately high winds (12 m/s) and a moist
atmosphere (high vapor and/or heavy clouds), the scattering process increases the reflected
37 GHz radiation by about 1 K for v-pol and 5 K for h-pol. At 7 GHz, the increase is much
less, being about 0.2 K for v-pol and 0.8 K for h-pol. The accuracy of the above approxima-
tion as compared to the theoretical computation is about 0.03 K and 0.2 K at 7 and 37 GHz,
respectively. Note that when the atmospheric absorption becomes very large (i.e., τ is
small), Ω tends to zero because the sky radiation for a completely opaque atmosphere is
2.7. Wind Direction Effects
The anisotropy of the sea-surface roughness produces a variation of the brightness tem-
perature versus wind direction, as discussed in Section 2.5. In the 19 to 37 GHz band, Wentz
 determined this wind direction signal using collocated SSM/I TB’s and buoy wind
vectors. At an incidence angle near 53°, the wind direction signal exhibits the following sec-
ond-order harmonic variation with wind direction:
∆E19−37 = γ 1 cos φ + γ 2 cos 2φ (63)
where ∆E is the change in the sea-surface emissivity and φ is the wind-direction angle rela-
tive to the azimuth-look angle. When φ = 0° (180°), the observation is upwind (downwind).
The subscript 19-37 denotes that the results are for the 19-37 GHz band. The amplitude co-
efficients γ1 and γ2 are found to be essentially the same for both 19 and 37 GHz. The coeffi-
cients are different for the two polarizations and do vary with wind speed as given below
γ 1V = 7.83 × 10 −4 W − 2.18 × 10 −5 W 2 (64a)
γ 2 V = −4.46 × 10 −4 W + 3.00 × 10 −5 W 2 (64b)
γ 1H = 1.20 × 10 −3 W − 8.57 × 10 −5 W 2 (65a)
γ 2 H = − 8.93 × 10 −4 W + 3.76 × 10 −5 W 2 (65b)
In Wentz , the wind direction signal was expressed in terms of a brightness tempera-
ture change rather than an emissivity change, and the wind speed was referenced to a 19.5 m
anemometer height. In the above equations, we have converted the Wentz  expres-
sions from ∆TB to ∆E and use a 10 m reference height for W.
Little is known about the wind direction signal for frequencies below 19 GHz. Some
very preliminary data from the Japanese AMSR aircraft simulations suggests that the signal
decreases with decreasing frequency. Other than this, there are no experimental data on the
variation of TB versus φ at 6.9 and 10.7 GHz. As an educated guess on what will be ob-
served at these lower frequencies we reduce the wind direction signal from its value at 19
GHz by a factor of 0.82 at 10.7 GHz and by a factor of 0.62 at 6.9 GHz.
The result for the wind direction signal from (64) and (65) should be regarded as prelim-
inary. Recent aircraft data Yueh et al.  as well as a first analysis of TMI measure-
ments suggest that at wind speeds below 8 m/s the wind direction signal is noticeably smaller
than the one obtained from (64) and (65), especially for the h-pol. A reanalysis of the direc-
tional signal using data from 5 SSM/I satellites between 1987 and 1999 as well as recent
TMI data is currently under way.
3. The Ocean Retrieval Algorithm
In general, there are three types of ocean retrieval algorithms:
1. Multiple linear regression algorithms
2. Non-linear, iterative algorithms
3. Post-launch in-situ regression algorithms
The first two types are physical algorithms in the sense that radiative transfer theory is used
in their derivation. The third type is purely statistical with little or no consideration of the
underlying physics. We now describe each of these algorithms and discuss their strengths
3.2 Multiple Linear Regression Algorithm
Consider a linear process in which a set of inputs denoted by the column vector X is
transformed to a set of outputs denoted by the column vector Y. The linear process is then
characterized by the matrix A that relates Y to X.
Y = AX (66)
The measurement of Y usually contains some noise ε and is denoted by
Y = Y + ε = AX + ε (67)
The retrieval problem is then to estimate X given Y . The most commonly used criteria for
estimating X is to find X such that the variance between Y and Y is minimized. Using this
criteria, one finds the well known least-squares solution:
X = (A TΞ−1A)−1 A TΞ−1Y (68)
where Ξ is the correlation matrix for the error vector ε. If the errors are uncorrelated, then Ξ
For our application, the system input vector X is the set of geophysical parameters P and
the output vector Y is the set of TB measurements. Note that X and Y can be non-linear
functions of P and TB, respectively without violating the requirement for linearity between X
and Y. For example, the relationship between TB and atmospheric parameters V and L can
be approximated by
TB ≈ TE 1 − R exp −2 sec θi A O + a V V + a L L gs (69)
where TE is an effective temperature of the ocean-atmosphere system which is relatively con-
ln( TE − TB ) = ln( RTE ) − 2 sec θi A O + a V V + a L L g (70)
From this we see that the relationship between TB and V, L can be linearized by transforming
from Y = TB to Y = ln(TE − TB). Wilheit and Chang  followed this approach and used
a value of 280 K for T E. As a further extension, Y can also include higher order terms such
as TB2 and TB37V TB23H.
Likewise, the input X can be a nonlinear transformation of the geophysical parameters P.
For example, the wind speed dependence of TB (i.e., ∂TB/∂W) increases with wind speed, and
the relationship can be made linear by the following transformation
W′ = W W < W1 (71a)
W ′ = W + M1 ( W − W1 ) 2
W1 ≤ W ≤ W2 (71b)
W ′ = M2 W − M3 W > W2 (71c)
This transformation represents two linear segments connected by a quadratic spline such that
the function and its first derivative are continuous.
Thus the requirement of linearity is not as constraining as it might first appear, and a
generalized linear statistical regression algorithm can be represented by
Pj = ℜ c 0 j + ∑ c ij ℑ( TBi )
N i =1 Q (72)
where ℑ and ℜ are linearizing functions. Subscript i denotes the AMSR channel (1 = 6.9V,
2 = 6.9H, etc.), and subscript j denotes the parameter to be retrieved (1 = TS, 2 = W, 3 = V, 4
= L). For AMSR, our initial design for the linear regression algorithm discussed in the next
section uses the following linearizing functions:
ℑ( TB ) = TB ν = 6.9 and 10.7 GHz (73a)
ℑ( TB ) = − ln(290 − TB ) ν = 18.7, 23.8, and 36.5 GHz (73b)
ℜ( X ) = X (74)
After testing the initial algorithm, we will experiment with additional linearizing functions,
such as the wind speed linearization given by (71).
In principle, the cij coefficients can be found from (68) given the A matrix and the error
correlation matrix Ξ. However, even after the linearizing functions are applied, the relation-
ship of Y versus X is not strictly linear, and the elements of A matrix are not constant, but
rather vary with P. One could find a linear approximation for the Y versus X relationship,
and then derive the cij coefficients from (68). However, we prefer the more direct approach
suggested by Wilheit and Chang  in which brightness temperatures are computed for
an ensemble of environmental scenes and then multiple linear regression is used to derive the
cij coefficients, as is discussed in the following section.
3.3. Derivation and Testing of the Linear Regression Algorithm
The derivation of the cij coefficients in the AMSR linear regression algorithm is shown in
Figure 5. A large ensemble of ocean-atmosphere scenes are first assembled. The specifica-
tion of the atmospheres comes from 42,195 quality-controlled radiosonde flights launched
5 Cloud Models
SST Randomly Varied for 0 to 30 C
Wind Speed Randomly Varied from 0 to 20 m/s
Wind Direction Randomly Varied from 0 to 360
Truth: Ts, W, V, L
Complete Radiative Transfer Model
Simulated AMSR TB's
Gaussian Noise Added
Withheld Data Set
Derive Coefficients for Multiple
Linear Regression Algorithm
Retrieved values for Ts, W, V, L
Evalulate Algorithm Peformance
Performance and Cross Talk Statistics
Fig. 5. Derivation and testing of the linear regression algorithm
from small islands during the 1987 to 1990 time period [Wentz, 1997]. One half of these ra-
diosonde flights are used for deriving the cij coefficients, and the other half is withheld for
testing the algorithm. A cloud layer of various columnar water densities ranging from 0 to
0.3 mm is superimposed on the radiosonde profiles. Underneath these simulated atmo-
spheres, we place a rough ocean surface. The sea-surface temperature TS is randomly varied
from 0 to 30 C, the wind speed W is randomly varied from 0 to 20 m/s, and the wind direc-
tion φ is randomly varied from 0 to 360°. About 400,000 scenes are generated in this man-
In nature, there is a strong correlation between TS and W. We could have incorporated
this correlation into the ensemble of the scene. For example, we could have discarded cases
of very cold water and very high water vapor, which never occur in nature. However, for
now we include these unrealistic cases in order to determine if the algorithm is truly capable
of separating the TS signal from the V signal.
Atmospheric brightness temperatures TBU and TBD and transmittance τ are computed from
the radiosonde + cloud profiles of T(h), p(h), ρV(h), and ρL(h) using equations (17), (18) and
(19). The reflectivity R of the rough sea surface is computed according to the equations giv-
en in Section 2.5, and the atmospheric radiation scattered from the sea surface T BΩ is com-
puted from (61). Wind direction effects are included as described in Section 2.7. Finally,
the brightness temperature TB as seen by AMSR is found by combining the atmospheric and
sea-surface components, as is expressed by (10).
Noise is added to the simulated AMSR TB’s. This noise represents the measurement er-
ror in the AMSR TB’s. The measurement error depends on the spatial resolution. At a 60-
km resolution, which is commensurate with the 6.9 GHz footprint, the measurement error is
0.1 K. A random number generator is used to produce Gaussian noise having a standard de-
viation of 0.1 K. This noise is added to the simulated T B’s. At this point in the simulation,
we could also add modeling error to the TB’s. Modeling error accounts for the difference be-
tween the model and nature. It is a very difficult parameter to determine since it involves
physical processes which are not sufficiently understood to be included in the current model.
For now, we are not including any modeling error in the simulations, but we will be investi-
gating this problem in the future.
Given the noise-added simulated TB’s, the standard multiple linear regression technique
is used to find the cij coefficients. The coefficients are found such that the rms difference be-
tween Pj and the true value for the specified environmental scene is minimized. For the ini-
tial set of simulations, we use all 10 lower frequency channels (i.e., 6.9, 10.7, 18.7, 23.8 and
36.5 GHz, dual polarization). Later on, we will investigate the utility of using a reduced set
The algorithm is tested by repeating the above process, only this time using the withheld
environmental scenes. The geophysical parameters TS, W, V, and L are computed from the
noise-added TB’s using equation (72). Statistics on the error in P i are accumulated. The re-
sults are shown in Figure 6. The solid line in the figure shows the mean retrieval error, and
the dashed lines show the one standard deviation envelope. The retrieval error for each of
the four parameters is plotted versus the four parameters in order to show the crosstalk error
0 30 0 20 0 70 0 .3
CLOUD DIF (MM)
VAPOR DIF (MM)
WIND DIF (M/S)
SST DIF (C)
0 30 0 20 0 70 0 .3
SST (C) WIND (M/S) VAPOR (MM) CLOUD (MM)
Fig 6. Preliminary results for the linear statistical regression algorithm for AMSR. The
solid line in the figure shows the mean retrieval error, and the dashed lines show the
one standard deviation envelope. The retrieval error for each of the four parameters is
plotted versus the four parameters in order to show the crosstalk error matrix. The di-
agonal in the crosstalk matrix verifies that the dynamic range of a given parameter is
correct, and the off-diagonal plots verifies that there is no crosstalk error in the re-
matrix. The diagonal in the crosstalk matrix verifies that the dynamic range of a given pa-
rameter is correct, and the off-diagonal plots verify that there is no crosstalk error in the re-
The results look quite good. There is a little crosstalk, but it is quite small. Table 9
gives the overall rms error for the retrievals. Wind direction variability is a major source of
error in the TS retrieval. When wind direction variability is removed from the simulations,
the TS retrieval error decreases to 0.3 C. The wind direction problem is further discussed in
Sections 1.5 and 4.3.
We again emphasize that these results are very preliminary. There is much more work to
do. For example, the cloud models need to be more variable and the performance of the rel-
atively simple LSR algorithm needs to be compared with the non-linear algorithm discussed
in the next section.
Table 9. Preliminary Estimate of Retrieval Error
Ocean Parameter Rms Error
Sea-Surface Temperature 0.58 C
Wind Speed 0.86 m/s
Columnar Water Vapor 0.57 mm
Columnar Cloud Water 0.017 mm
3.4. Non-Linear, Iterative Algorithm
The major shortcoming of the multiple linear regression algorithm is that the non-lineari-
ties in the TB versus P relationship are handled in an ad hoc manner. The linearization func-
tions are only approximations, and the inclusion of second order terms such as TB2 and TB37V
TB23H do not really describe the inverse of the TB versus P relationship. A more rigorous
treatment of the non-linearity problem is to express the T B versus P relationship in terms of a
non-linear model function F(P), and then invert the following set of equations
TBi = Fi (P ) + ε i (75)
where subscript i denotes the observation number and εi is the measurement noise. The num-
ber of observations must be equal to or greater than the number of unknown parameters (i.e.,
the number of elements in P). For each set of AMSR observations, equations (75) are in-
verted to yield P. This method is much more numerically intensive than the linear regression
algorithm in which there is a fixed relationship between P and TB. However, given today’s
computers, the computational burden is no longer a problem.
Equation (75) is solved using an extension of Newton’s iterative method. In Newton’s
method, the model function is expressed as a Taylor expansion:
TBi = Fi ( P ) + ∑ Pj − Pj i
+ O2 + ε i (76)
j=1 ∂ j P
where P is a first guess value for P and O2 represents the higher order terms in the expan-
sion. This system of simultaneous equations is written in matrix form as
∆TB = Α ∆P + O2 + ε (77)
where A is a matrix of i × j elements and ∆TB, ∆P, and ε are column vectors. The elements
of A, ∆TB, and ∆P are
A ij = (78)
∆TBi = TBi − Fi ( P ) (79)
∆Pj = Pj − Pj (80)
Equation (77) is solved by ignoring the higher order terms (i.e., by setting O2 to zero), and
the solution is
P = P + (A TΞ−1A)−1 A TΞ−1∆TB (81)
where Ξ is the error correlation matrix. This procedure is then repeated with P from (81) re-
placing P , and several such iterations are performed. For the no-noise case ( ε = 0), Ξ drops
out of the formulation and an exact solution is obtained when ∆TB goes to zero. For the
noise case, a solution is found when ∆TB reaches some constant minimum value.
The solution of P can be constrained by the inclusion of a priori information. This is ac-
complished by including additional equations in (77). For example, if ancillary information
on wind direction were available, then the following equation could be added to (77)
φ = φ + εφ (82)
where φ is the a priori estimate of φ and ε φ is the rms uncertainty in that estimate. Similar
constraining equations can be included for other types of information such as the vertical dis-
tribution of water vapor and air temperature.
In general, there is no guarantee that a solution will be found using this method. Further-
more, if a solution is found, there is no guarantee that it is an unique solution. However for
the case of AMSR, the relationships between P and TB are quasi-linear in that ∂TB/∂P > 0 for
all channels except 36.5 GHz in cold water, for which ∂TB/∂TS is < 0. Experience has shown
that a solution is nearly always found. It also appears that this solution is unique, but this
needs to be verified.
We have been assuming that the TB versus P relationship can be exactly described by a
non-linear model function F. In this case, the non-linear, iterative algorithm has the distinct
advantage of finding the exact solution. In comparison, the P found by the linear regression
algorithm would be in error by some degree due to the non-linearities. However, in practice
it is not possible to exactly represent the TB versus P relationship in terms a model function
F(P). For example, the TB not only depends on the columnar content of water vapor but also
on vertical distribution of the vapor. Thus, some approximations need to be made when go-
ing from the integral equations of radiative transfer to a simplified model function F(P).
These assumptions were discussed in length in Section 2. In the derivation of the linear re-
gression algorithm, the complete integral formulation of the radiative transfer theory is used,
and there is no need for the simplifying assumptions.
In comparing the two types of algorithms, there is a tradeoff between errors due to non-
linearities in the linear regression algorithm and errors due to simplifying assumptions in the
non-linear, iterative algorithm. Our plan is to develop and test both types of algorithms in
parallel, compare their relative performance, and then select one or the other.
3.5. Post-Launch In-Situ Regression Algorithm
After AMSR is launched, purely statistical algorithms can be developed by collocating
the AMSR TB’s with selected in-situ sites. A simple least-squares regression is then found
that relates the in situ parameter to the TB’s. The mathematical form of this type of algo-
rithm is identical to the linear regression algorithm given by (72). The difference is that the
cij coefficients are not derived from radiative transfer theory, but rather from the regression
to the in situ data. Examples of this type of algorithm are the Goodberlet et al.  SSM/
I wind algorithm and the Alishouse et al.  SSM/I water vapor algorithm.
The strength of the purely statistical algorithm is that it does not require a radiative trans-
fer model, and hence it is not affected by modeling errors. The weaknesses are:
1. The algorithm for AMSR cannot be developed until after launch.
2. Large in situ data sets covering the full range of global conditions must be assembled and
collocated with the AMSR observations.
3. The purely statistical algorithm is keyed to specific sensor parameters such as frequency
and incidence angle. For example, none of the algorithms developed for SSM/I can be ap-
plied to AMSR. In contrast, SSM/I algorithms based on radiative transfer theory can be in-
terpolated to the new AMSR frequencies and incidence angle.
4. Cross-talk among the various geophysical parameters is a problem for the statistical algo-
rithm. For example, consider sea-surface temperature TS and water vapor V which are high-
ly correlated on a global scale. A purely statistical algorithm will mimic this correlation and
will generate a TS product that is always highly correlated with V. In nature, when the true
V changes and TS remains constant (i.e., a weather system passing by), the statistical algo-
rithm will erroneously report a change in TS.
5. For the case of cloud water retrieval, for which there is no reliable in situ data, this type
of algorithm cannot be used.
We think it is a mistake to ignore the physics when developing an algorithm. It may be
the case that relatively simple regressions can be used to retrieve some of the parameters.
However, it is important that these regressions be understood in the context of radiative
transfer theory. Thus, after AMSR is launched and the collocated in situ data are available,
we will calibrate the pre-launch algorithm by making small adjustments to the radiative
transfer model rather than developing purely statistical algorithms. This calibration activity
is discussed in the Section 5.
3.6. Incidence Angle Variations
The retrieval of sea-surface temperature and wind speed are sensitive to incidence angle
variations. A 1° error in specifying θi produces a 6 C error in T S and a 5 m/s error in W.
Thus, it is crucial that the incidence angle be accurately known and that the retrieval algo-
rithm accounts for incidence angle variations.
The pointing knowledge for the PM platform is specified to be 0.03°/axis. This figure is
the 3-standard deviation error in the knowledge of the roll, pitch, and yaw. Yaw variations
do not affect the incidence angle, but roll and pitch do. The corresponding 3-standard devia-
tion error in incidence angle is approximately 0.05°. The retrieval accuracy for the geophys-
ical parameters are in terms of a 1-standard deviation error, so we convert the incidence an-
gle error to a 1-standard deviation error of 0.016°, and this results in a 0.1 C error in the T S
retrieval and a 0.1 m/s error in the W retrieval. The specification of pointing knowledge for
the PM platform is, therefore, sufficient. However, the pointing knowledge of the AMSR in-
strument is yet to be specified. We will be paying close attention to this instrument specifi-
In the non-linear, iterative algorithm, incidence angle is an explicit parameter in the mod-
el function, and hence θi variations are easily handled by simply assigning a value to θi be-
fore doing the inversion process. There are two possible methods for handling incidence an-
gle variation in the linear regression algorithm. First, include incidence angle as an addition-
al term in the regression or second, normalize the TB’s to some constant incidence angle, say
55°, before applying the regression. This normalization is expressed by
TB (55o ) = TB (θi ) + µ θ i − 55o h (83)
where µ represents the derivative ∂TB/∂θi, which depends on the TS, W, V, and L. We find
that µ can be accurately approximated by a TB regression of the type given by (73). This
method works well when the incidence angle variations are ± 1° or less, which should be the
case for AMSR.
4. Level-2 Data Processing Issues
4.1. Retrievals at Different Spatial Resolutions
Figure 7 shows the data processing done by the Level-2 ocean algorithm. The input is
the Level-2A data files, which contain brightness temperatures at four base resolutions:
1. Low (L): 6.9 GHz antenna pattern, approximately 58 km resolution
2. Medium (M): 10.7 GHz antenna pattern, approximately 38 km resolution
3. High (H): 18.7 GHz antenna pattern, approximately 24 km resolution
4. Very High (VH): 36.5 GHz antenna pattern, approximately 13 km resolution
For each resolution, all higher frequency channels are averaged down to the base resolution.
In this way, all channels within a base resolution set are at a common spatial resolution. The
four base resolutions are centered on the observation boresight points, which for AMSR are
nearly coincident for all channels other than 89.5 GHz. The ocean algorithm does not use
89.5 GHz. The boresight points are spaced 10 km along the scan, and the scans are separated
by 10 km in the along-track direction. For the H and VH resolutions, the Level-2A data set
contains TB’s for every boresight point. That is to say, the H and VH Level-2A T B’s are on a
10-km scan-oriented grid system. For the L and M resolutions, a sparse grid that corre-
sponds to every other observation along a scan and every other scan is used for Level-2A.
Thus the L and M grid has a 20-km spacing.
The data processing is done by separate modules that correspond to the L, M, V, and VH
resolutions. Since the TS retrievals require the 6.9 GHz channel, the L module’s function is
find TS. There is some TS sensitivity at 10.7 GHz, and as a special product, the M module
finds TS at a higher resolution of 38 km. However, the primary function of the M module is
to retrieve wind speed. The H module’s primary function is to retrieve the atmospheric pa-
rameters V and L. In addition, the H module also computes a high resolution wind, which is
a special product. The VH module just retrieves the cloud liquid water parameter, which is
used to flag rain.
The four standard products coming from this processing are:
1. Sea-surface temperature at a resolution of 58 km
2. Wind speed at a resolution of 38 km
3. Water vapor at a resolution of 24 km
4. Cloud liquid water at a resolution of 13 km
And the special products are:
1. Sea-surface temperature at a resolution of 38 km
2. Wind speed at a resolution of 24 km
All of these products are output on the 10-km Level-2A grid. This requires that TS and W,
which are retrieved on the 20-km grid, be remapped to the 10-km grid. Thus T S and W are
over-sampled. However, we think using the same output grid for all four parameters is
preferable from a user’s standpoint, even if some parameters are over-sampled.
Lo-Res. Level-2A TB
Med-Res. Level-2A TB
Remap to Remap to
10-km grid 10-km grid Hi-Res. Level-2A TB
Very Hi. Res. Level-2A TB
Lo-Res. Ts Med-Res. Ts, W Hi-Res. W, V, L VHi-Res. L
Note: Med-Res. Ts and Rain-Flag
Hi-Res. W are Special Products Module
Fig. 7. Data processing flow for ocean algorithm
The first step in the data processing is to compute sea-surface temperature TS. This is
done by the L module which executes the retrieval algorithm described in the previous sec-
tion. The baseline version of the algorithm uses all AMSR channels except the 89 GHz
channels. Later, we may trim down the number of channels if our sensitivity analysis indi-
cates certain channels are not needed. Note that the non-linear, iterative algorithm simulta-
neously finds W, V, and L along with TS, but these other retrievals are recomputed at higher
spatial resolutions by modules M, H, and VH.
The second step is to compute the medium resolution wind speed, which is done by mod-
ule M. In this case, only the 10.7 18.7, 23.8, and 36.5 GHz channels are used. Module M
also retrieves TS at the spatial resolution of 38 km. This higher resolution T S is a special
product and will only be useful when the sea-surface temperature is above 15 C. For cold
water, the 10.7-GHz ∂TB/∂TS is too small to retrieve TS. In order to compute W, module M
requires the TS retrieval from module L. For the linear regression algorithm, the TS retrieval
is included as an additional term in the regression for W. For the non-linear, iterative algo-
rithm, the information of the TS retrieval is included as an additional equation:
TS = TS + ε TS (84)
where TS is the higher resolution sea-surface temperature, TS is the estimated lower resolu-
tion TS coming from module L, and ε TS is the rms error of the estimate. Equation (84) pro-
vides the means to vary the way in which TS is assimilated. For example, in cold water, ε TS
can be set to zero (or near zero), which forces the algorithm to retrieve a value of T S that
equals the low resolution value. This is a good choice for cold water because ∂TB/∂TS at
10.7 GHz is too small to retrieve TS. In warm water, ε TS can be set to 1 or 2 C. In this case,
the algorithm is allowed to retrieve a high resolution TS that is not necessarily the same as
the low resolution TS, but which is constrained to be relatively close to the low resolution
value. This is an example of the flexibility and adaptability of the non-linear algorithm.
The high resolution module is then executed. Module H retrieves the columnar water va-
por V and columnar liquid water L. In addition, a high-resolution wind speed is also found.
Module H only uses the 18.7, 23.8, and 36.5 GHz channels. The module requires the sea-
surface temperature and wind estimates coming from modules L and M. The TS and W esti-
mates are assimilated into module H in a manner analogous to the way the T S estimate is as-
similated into module M.
The very high resolution 36.5 GHz observations are then processed by module VH. In
this case, module VH only finds the cloud liquid water L. The spatial resolution of these re-
trievals is 13 km. The retrieval algorithm requires the estimates of TS, W, and V from mod-
ules L, M, and H.
The final step is to perform rain flagging. The rain-flag module searches for rain within
the L, M, and H footprints. The VH retrievals of L are used as an indicator of rain. Past in-
vestigations [Wentz, 1990; Wentz and Spencer, 1997] have shown that a threshold of L =
0.18 mm is a reliable indicator of rain. The amount of rain in each of the three footprints is
determined and the appropriate flag is set. The rain-flag module must search over 15 AMSR
scans in order to cover the L footprint out to the first null of the antenna pattern.
4.2 Granules and Metadata
The Level-2 ocean products that are produced for each 1.5-second AMSR scan are listed
in Table 10. There are 196 observations taken each scan. The products are stored as un-
signed 2-byte positive integers, except for time, that is stored as an 8-byte integer and the or-
bit number (which includes a fractional part) that is stored as a 4-byte integer. To convert
the integers to geophysical units, they are multiplied by the scale factor and then the offset is
added. The data rate is 18,496 bits/second, which is 14 megabytes (MB) per orbit or 200
The various Level-2 ocean products are closely tied together, and we therefore define a
granule of ocean data as one orbit of all the parameters listed in Table 10. Time and location
information are always required for each product. The incidence angle and azimuth angles
are included so that corrections can be applied to the products after Level-2 processing. For
example, if wind direction variability proves to be a problem for the TS retrieval (see next
section), then a wind-direction database can be later used to correct the problem. The Earth
azimuth angle will be required to perform this correction. The four geophysical retrievals
are interrelated. Many science applications such as air-sea interaction studies require all four
parameters. Also, the atmospheric parameters V and L provide information on the accuracy
of the sea-surface parameters TS and W. Thus we think all of these parameters should be
stored together as one granule.
A full description of each product will be included as metadata attached to the granule.
The metadata defines each product, provides advice on using the products, and discusses the
accuracy and limitations of the products. For example, the metadata will point out that the
sea-surface temperature and wind speed retrievals will be of degraded accuracy when rain is
Table 10. AMSR Level-2 Ocean Data Record
Data Item No. Samples No. Bits Scale Factor Offset
Time (sec) 1 64 1 0.0
Orbit Number 1 32 1 0.0
Earth incidence angle (deg) 196 3136 0.01 0.0
Earth azimuth angle (deg) 196 3136 0.01 0.0
Latitude (deg) 196 3136 0.01 0.0
Longitude (deg) 196 3136 0.01 0.0
Surface type and QC flag 196 3136 1 0.0
Sea-Surface Temperature TS (K) 196 3136 0.01 -5.0
Wind Speed W (m/s) 196 3136 0.01 -4.0
Water Vapor V (m/s) 196 3136 0.01 -2.0
Cloud Liquid Water L (mm) 196 3136 0.001 -0.1
Total bits in record 28320
4.3. Requirements for Ancillary Data Sets
The AMSR data processing has minimal requirements for ancillary data sets, with one
possible exception: wind direction information. If the error in the TS retrieval due to wind
direction variations proves to be unacceptably large, then a wind direction database will be
required. This possibility is discussed below. All other ancillary data sets are small static ta-
bles that are easily implemented. These data sets are listed in Table 11.
The land-coast-ocean mask is a map that indicates a particular location is either all land,
all ocean, or mixed land and ocean. This map is used to exclude observations that are con-
taminated by the hot thermal emission of land. The sea-surface temperature climatology is
used for retrieving W, V, and L when the T S retrieval from the 6.9 GHz channels is not
available. For example, a retrieved value of TS is not available near coasts and in rainy ar-
eas. The sea-surface salinity map is required for the accurate retrieval of T S. In the open
ocean, the salinity varies from about 32 to 37 parts/thousand. The 6.9 GHz v-pol channel is
most sensitive to salinity variations. In warm water a 5 parts/thousand change in salinity
corresponds to a 0.3 K change in the 6.9V TB. To achieve a rms accuracy of 0.5 C in the TS
retrieval, the salinity will need to be known to an accuracy of about 2 parts/thousand. The
sea-ice climatology mask indicates when a particular location is in an area of possible sea
ice. This ice mask is based on 20 years of microwave radiometer (SMMR and SSM/I) sea
ice observations. The 20-year maximum extent of sea ice was determined, and then a 100-
km buffer was added to ensure that observations outside the mask would be free of ice. The
one exception is the occasional large iceberg that moves outside the ice mask. The ice mask
is used as a quality control measure to flag retrievals that may be contaminated by emission
of sea ice.
Table 11. Ancillary Data Sets Required by Level-2 Ocean Algorithm
Parameter Temporal Resolution Spatial Resolution Source
Land-Coast-Ocean Mask not applicable 0.1° lat. by 0.1° long. C.I.A.
Sea-Surface Temperature Climatology monthly 2° lat. by 2° long. Shea et al. 
Sea-Surface Salinity Climatology monthly 2° lat. by 2° long. To be determined
Sea Ice Climatology Mask monthly 1° lat. by 1° long. SSM/I Analysis
Wind direction variability is a major source of error in the T S retrieval. The simulation
studies discussed in Section 3.3 indicate that in the absence of wind direction variability, T S
can be retrieved to an accuracy of 0.3 C. When wind direction variability is included in the
simulation, the rms error goes up to 0.6 C. Currently, there is considerable uncertainty of the
magnitude of the wind direction TB signal at 6.9 GHz. The flights of the TRMM 10.7-GHz
radiometer provide valuable information on the wind direction TB signal at the lower fre-
quencies. If the wind direction variation of the lower frequency T B proves to be a dominant
source of error, then we will need to make a correction to the T S retrieval based on some
wind direction database. There are two possible sources of wind direction information. First
is NCEP and ECMWF surface analyses, and the second is the SeaWind scatterometer.
4.4. Computer Resources and Programming Standards
The Level-2 processing of the ocean algorithm will require modest computer resources.
The SSM/I Level-2 processing can be used as a benchmark. The SSM/I Level-2 processing
is done on a Pentium Pro-200™ at Remote Sensing Systems. It takes about 1 day to process
one-month of SSM/I data. The AMSR Level-2 processing should be no more than a factor
of 10 greater than that for SSM/I. We expect that desktop workstations will continue to in-
crease in performance at a rate of doubling every 2 years. Thus, in the year 2001 when the
PM-AMSR data becomes available, we expect that a state-of-the-art desktop workstation
will be able to process one-month of AMSR data in one day.
The Level-2 processing will ingest one complete orbit of Level-2A data, excluding the
89.5 GHz observations. This will require about 50 megabytes (MB) of memory to store the
input data and 30 MB to store the output data. An additional 64 MB will be more than
enough for code, tables, and temporary storage. Thus, a workstation with 256 MB of memo-
ry will be more than adequate.
The source code for the algorithm will be written in Fortran 90, and all required SDP
Toolkit functions will be implemented.
5. Validation for the Ocean Products Suite
The final, prelaunch ocean algorithm for the EOS-PM AMSR will have benefited from
two separate calibration and validation activities: SSM/I and TMI. We originally planed
to use the AMSR aboard the ADEOS-2 spacecraft to further develop and test the AMSR-E
ocean algorithm. Now that the ADEOS-2 launch date has slipped to 2001, this is no longer
possible. We are placing more attention on the TMI data set for AMSR algorithm develop-
ment. However, the final specification of the 6.9 GHz emissivity will need to be done after
the AMSR-E launch. We expect that the 6.9 GHz emissivity can be relatively quickly speci-
fied given 1 to 3 months of AMSR observations. After specifying the 6.9 GHz emissivity,
we expect that the AMSR algorithm will perform very well and will provide the scientific
community with accurate ocean products. However, there are two caveats that need to be
considered. First, it is not possible to absolutely calibrate satellite microwave radiometers to
better than 1 to 2 K. In other words, there will probably be a constant TB bias of 1 to 2 K be-
tween SSM/I, TMI, and the two AMSR’s. Fortunately, this bias is easily modeled in terms
of either an additive or multiplicative offset for each channel. Thus the first caveat is that TB
offsets need to be derived after launch before accurate retrievals can be realized. The second
caveat is that some fine tuning of the model coefficients will probably be required in order to
maximize the retrieval accuracy.
Given these caveats, we have developed a two-step post-launch calibration/validation (cal/
val) plan. First, in order to determine the 6.9 GHz emissivity and the T B offsets, we will per-
form a 3-month, quick-look cal/val. The objective of the 3-month cal/val is to quickly im-
plement the emissivity and TB offsets so that reasonably accurate ocean products can be de-
livered to the scientific community soon after launch. Also, the quick-look calibration may
identify other obvious problems in the algorithm that can be corrected. A more thorough 1-
year investigation will then be conducted, a precision calibration will be done, and the algo-
rithm will be updated. The updated algorithm will represent the Version 2 post-launch
AMSR algorithm, and we anticipate that it will be used to process data for several years.
Once the Version-2 software is implemented, we will begin several research activities aimed
towards extracting the maximum information content from the AMSR observations. Our
AMSR investigation will conclude with an optimal algorithm for retrospective processing of
the AMSR data.
The calibration and validation of the first 3 ocean products (T S, W, and V) will be based
on intercomparisons with buoy and radiosonde observations and on TS retrievals coming
from IR satellite sensors. With respect to cloud liquid water, there are no reliable ancillary
data sets for calibration or validation. In this case, we will rely on a histogram analysis simi-
lar to that done by Wentz . The details of the cal/val activity for each ocean parameter
will now be discussed.
5.2 Sea-Surface Temperature Validation
The AMSR TS will be validated by comparisons with buoy measurements and IR SST
products coming from the AVHRR series of instruments onboard the NOAA polar-orbiting
satellite series. The IR SST products rely on several AVHRR channels, primarily channel 3
(3.6 to 3.9 µm), channel 4 (10.3-11.3 µm), and channel 5 (11.5 to 12.5 µm). The use of
multiple channels allows for cloud detection in the retrieval process. Several algorithms to
retrieve SST from AVHRR and other IR sensors have been developed, including the multi-
channel (MC SST) [McClain, 1981], and the non-linear (NL SST), used to produce the
AVHRR Pathfinder dataset [Vazquez, 1999], as well as experimental algorithms that include
measurements of columnar water vapor from SSM/I. These algorithms are used to generate
some of the data products summarized in Table 12. A review of the various algorithms is
given by Barton . The major drawback to the IR SST retrievals is interference due to
spatial and temporal fluctuations in the atmosphere. Clouds, aerosols, and water vapor
[Emery et al., 1994] all interfere with the measurement of SST, since emittance from these
typically cooler layers reduce the inferred brightness temperature (but warm clouds over a
boundary layer inversion can have the opposite effect). Thus in doing comparisons with
AMSR, care will be taken to avoid cloudy areas.
Table 12. Some of the available SST products.
SST Data Set Acronym Temporal Res. Spatial Res.
Reynolds Optimum Interpolation SST Reynolds SST Weekly 100km
AVHRR Multi-Channel SST MC SST Weekly, Monthly 18 km
AVHRR Pathfinder v4.1 SST PF SST Daily, Monthly 9, 18, 54km
NESDIS SST Analyses NESDIS SST Daily 8 km
GOES SST GOES SST Hourly 4 km
TMI SST TMI SST Daily 50 km
The AMSR SST retrievals will also be validated by direct comparisons with ocean buoys.
A rather extensive ocean buoy network is currently deployed in the Atlantic and Pacific
Oceans. The Tropical Atmospheric Ocean (TAO) buoy array, concieved in the early 1980s
and completed in 1994, consists of approximately 70 buoys located in the tropical Pacific
between 8°N and 8°S. The new Pilot Research Moored Array in the Tropical Atlantic
(PIRATA) is currently being implemented between 10 south and 15 north latitude. This
array of 12 buoys is being opearted and managed by the Climate Variability (CLIVAR)
group within the World Climate Research Program using multi-national cooperation. A third
buoy dataset consists of a variety of buoy platforms and C-MAN stations located along US
coastlines operated by the National Data Buoy Center (NDBC). In comparing the satellite
and buoy measurements, two important effects need to be considered. First is the spatial-
temporal mismatch between the buoy point observation and the satellite 50-km footprint.
Second is the difference between the ocean skin temperature at 1 mm depth and the tempera-
ture at 1 m depth measured by the buoy. Both of these effects will contribute to the observed
difference between these two different types of observations. A list of the NDBC buoys in
given in Table 13 and the location of the TAO array and the NDBC buoys is shown in Figure
Table 13. NDBC Moored Buoy Open Water Locations as of July 1996
WMO Number Latitude East Longitude General Location
41001 34.7 287.4 E. Hatteras
41002 32.3 284.8 S. Hatteras
41004 32.5 280.9 E. Charleston
41006 29.3 282.7 E. Daytona
41009 28.5 279.8 Canaveral
41010 28.9 281.5 E. Canaveral
41015 35.4 284.9 Cape Hatteras E
41016 24.6 283.5 Eleuthera
41018 15.0 285.0 Central Caribbean
41019 29.0 289.0 American Basin
42001 25.9 270.3 Mid Gulf of Mexico
42002 25.9 266.4 W. Gulf of Mexico
42003 25.9 274.1 E. Gulf of Mexico
42019 27.9 265.0 Lanelle
42020 27.0 263.5 Eileen
42035 29.2 265.6 Galveston
42036 28.5 275.5 S. Apalachicola
42037 24.5 278.6 Univ. of Miami
42039 28.8 274.0 NE Gulf of Mexico
42040 29.2 271.7 E. Miss River Delta
44004 38.5 289.3 Hotel
44005 42.9 291.1 Gulf of Maine
44006 36.3 284.5 Sandy Duck
44008 40.5 290.6 Nantucket
44009 38.5 285.3 Delaware Bay
44010 36.0 285.0 Sandy Duck
44011 41.1 293.4 Georges Bank
44014 36.6 285.2 Virginia Beach
44019 36.4 284.8 Sandy Duck
44025 40.3 286.8 Long Island
46001 56.3 211.8 Gulf of Alaska
46002 42.5 229.7 Oregon
46003 51.9 204.1 S. Aleutians
46005 46.1 229.0 Washington
46006 40.9 222.5 S.E. Papa
46025 33.7 240.9 Catalina Rdg
46028 35.8 238.1 C San Martin
46035 57.0 182.3 Bering Sea
46050 44.6 235.5 Stonewall Bank
46059 38.0 230.0 Boutelle Seamount
46061 60.2 213.2 Hinchinbrook
46147 51.8 228.8 S. Cape St. James
51001 23.4 197.7 N.W. Hawaii
51002 17.2 202.2 S.W. Hawaii
51003 19.1 199.2 W. Hawaii
51004 17.4 207.5 S.E. Hawaii
51026 21.4 203.1 N. Molokai
Fig. 8. Locations of data buoys
5.3 Wind Speed Validation
The chosen method of validation for the AMSR wind speed product is by intercomparisons
with wind observations of moored buoys deployed in the open ocean discussed above. The
NDBC buoys measure barometric pressure, wind direction, wind speed, wind gust, air and sea
temperature, and wave energy spectra (i.e., significant wave height, dominant wave period, and
average wave period). Wind speed and direction is measured during an 8 minute period prior to
the hour of report. Exactly when the data is collected prior to report and the height of the
anemometer depends on the type of payload on the moored buoy. These buoys are located pri-
marily in the coastal and offshore waters of the continental United States, the Pacific Ocean
around Hawaii, and from the Bering Sea to the South Pacific. In addition, there are about 50
coastal C-man stations that report hourly winds averaged over 2 minutes. The quality checked
hourly buoy and C-man measurements are available by anonymous ftp from NOAA computers.
Table 13 outlines the location of the NDBC moored buoys in service as of July 1996. These lo-
cations are mapped in Figure 8.
The 70 moored-buoy TOGA/TAO array covers the tropical Pacific ocean. These buoys
are placed at approximately 10 to 15 degree longitude intervals and 2° to 3° degree latitude
intervals. They measure air temperature, relative humidity, surface winds, T S, and
subsurface temperature to 500 meters. Wind measurements are made at a height of 4 m for 6
minutes centered on the hour and are vector averaged to derive the hourly value reported.
To conserve battery power, hourly data is transmitted only 8 hours each day, 0600 to 1000
and 1200 to 1600 buoy local time. Three to four hours of TS and wind data are available in
near-real time from the GTS. These data are considered preliminary until the buoy is
serviced and the stored hourly data is processed. This occurs approximately once each year.
Figure 9 includes the TAO buoy network.
The anemometer heights z for the buoys and C-man stations vary. The NDBC moored
buoys in general have z equaling 5 or 10 m, but some of the C-man stations have anemome-
ters as high as 60 m. The PMEL anemometers are at 3.8 m above the sea surface. All buoy
winds WB will be normalized to an equivalent anemometer height of 10 m (1000 cm) assum-
ing a logarithmic wind profile.
WB,10M = [ln(1000/h0)/ln(h/h0)] WB,Z (85)
where h0 is the surface roughness length, which equals 1.52×10−2 cm assuming a drag
coefficient of 1.3×10−3 [Peixoto and Oort, 1992].
The buoy data sets will undergo quality check procedures, including checks for missing data,
repeated data, blank fields, and out-of-bounds data. A time interpretive collocation program will
calculate the wind speed at the time of the nearest satellite overpass, as is described in Wentz .
5.4 Water Vapor Validation
The international radiosonde network will be used to validate the AMSR water vapor
product. Radiosonde data are available from several sources, including NCEP, NCDC, and
NCAR. A radiosonde consists of instruments which measure temperature, pressure, and
humidity as they are carried aloft by a helium balloon. In many locations throughout the world
radiosondes are launched twice each day (00Z and 12Z). To compare columnar water vapor
over ocean regions, only stations on small islands or ships are used. A preliminary list of 56
radiosonde stations currently operating on small islands are listed in Table 14 and are displayed
in Figure 9.
Quality control measures will include discarding incomplete or inconsistent soundings,
soundings without a surface level report, soundings with fewer than a minimal number of
levels, and those with spikes in the temperature or water vapor pressure profiles. These
measures will reduce the size of the available data set. In addition, corrections or
normalizations among the various types of sensors and sensor configurations will be required
since the radiosonde data are from different stations and countries. A collocation program will
be used to find the AMSR measurements within a specific space and time of each radiosonde
sounding. The details of collocating radiosondes with satellite observation and the associated
quality control procedures are given by Alishouse et al.  and Wentz .
Table 14. Island Radiosonde Station Locations as of September 1996
WMO No. Name Latitude East Longitude Area (km2)
1001 JAN MAYEN 70.93 351.33 373
1028 BJORNOYA 74.52 19.02 179
8594 SAL 16.73 337.05
43311 AMINI 11.12 72.73
43369 MINICOY 8.30 73.00
46810 PRATAS IS. 20.70 116.72
47678 HACHIJA JIMA 33.12 139.78 70
47918 ISHIGAKIJIMA 24.33 124.17 215
47945 MINAMIDAITO JIMA 25.83 131.23 47
47971 CHICHI JIMA 27.08 142.18 25
47991 MARCUS IS. 24.30 153.97 3
59981 XISHA IS. 16.83 112.33
61901 ST. HELENA -15.96 354.30 122
61902 ASCENSION IS. -7.97 345.96 88
61967 DIEGO GARCIA -7.35 72.48 152
61996 I. N. AMSTERDAM -37.80 77.53 62
63985 SEYCHELLES INTL -4.67 55.52 23
68906 GOUGH IS. -40.35 350.12 83
68994 MARION IS -46.88 37.87 388
70308 ST. PAUL IS. 57.15 189.79 91
70414 SHEMYA IS. 52.72 174.10 21
71600 SABLE IS. 43.93 299.98 8
78016 KINDLEY FIELD 32.37 295.32 53
78384 ROBERTS FLD. 19.30 278.63 183
78866 SAN MAARTEN 18.05 296.89 85
78954 BARBADOS 13.07 300.50 431
80001 ISLA SAN ANDREAS 12.58 278.30 21
82400 FERNANDO DE NORONHA -3.85 327.58 4
83650 TRINDADE IS. -20.50 330.68 10
85469 EASTER IS. -27.17 250.57 117
91066 MIDWAY 28.22 182.65 15
91245 WAKE IS. 19.28 166.65 8
91275 JOHNSTON IS. 16.73 190.49 1
91334 TRUK 7.47 151.85 118
91348 PONAPE/CAROLINE IS. 6.96 158.22 68
91366 KWAJALEIN 8.72 167.73 16
91376 MAJURO 7.03 171.38 10
91408 KOROR 7.33 134.48 8
91413 YAP 9.48 138.08 54
91610 TARAWA 13.05 172.92 23
91643 FUNAFUTI -8.52 179.22 3
91765 PAGO PAGO -14.33 189.29 135
91801 PENRHYN -9.00 201.95 10
91843 COOK ISLES -21.20 200.19 218
91925 ATUONA -9.82 220.99 200
91944 HAO -18.06 219.05 92
91948 RIKITEA -23.13 225.04 31
91952 MUROROA -21.81 221.19
91958 AUSTRAL IS. -27.61 215.67 47
93944 CAMPBELL IS. -52.55 169.15 17
93997 KERMADEC IS -29.25 182.09 34
94299 WILLIS IS. -16.30 149.98
94996 NORFOLK IS. -29.03 167.93 34
94995 LORD HOWE IS. -31.53 159.07 2
94998 MACQUARIE IS. -54.48 158.93 109
96996 COCOS IS. -12.18 96.82 14
Fig. 9. Radiosonde stations on small islands.
5.5 Cloud Water Validation
Microwave radiometry is probably the most accurate technology for measuring the
vertically integrated cloud liquid water L. In the 18 to 37 GHz band, clouds are semi-
transparent and the absorption by the entire column of liquid water can be measured. Apart
from using upward-looking radiometers to calibrate downward-looking radiometers (or vise
versa), there are no other calibration sources for L. Several nations (e.g., The Netherlands)
maintain upward looking radiometers or routinely make aircraft flights (e.g., Australia) to
measure L in support of their meteorological operations. These data sets are increasingly made
available to the scientific community over the Internet. However, the comparison L inferred
from upward looking radiometers with that inferred from downward looking satellite
radiometers has limited utility. The great spatial and temporal variability of clouds makes such
comparisons difficult. Also, the major problem in calibrating L is in obtaining accurate
retrievals over the full range of global conditions. There are not enough upward looking
radiometers to do this. Finally, when differences arise, it will be difficult to determine which
radiometer system is at fault.
We prefer to use the statistical histogram method described by Wentz . This tech-
nique is illustrated in Figure 10. We assume the probability density function (pdf) for the
true cloud water observed by AMSR has a maximum at L = 0 and rapidly decays similar to
an exponential pdf as L increases. The pdf for the retrieved L will look similar, but retrieval
error will tend to smear out the sharp peak at L = 0. Simulations in which Gaussian noise is
added to a random deviate having an exponential pdf show that the left-side, half-power
point of the pdf for the noise-add L is located at L = 0. Thus we require that histograms of
the L retrievals are aligned such that the half-power point of the left-side is at L = 0. Fur-
thermore, we require this condition be met for all TS, W, and V.
For example, the top plot in Figure 10 shows 6 histograms of L retrieved from SSM/I.
The 6 histograms correspond to 6 different ranges of TS (i.e., 0-5 C, 5-10 C, ..., 25-30 C).
The middle and bottom plots show analogous results for wind and water vapor groupings.
The peak of the pdf's is near L = 0.025 mm. At L = 0, all histograms are about half the peak
value. The misalignment among the 6 histograms is about ±0.005 mm. We use the width of
this half power point ( i.e., 0.025 mm) as an indicator of the rms error in L.
This procedure is effective in eliminating the bias and crosstalk error in the L retrieval,
and we consider it the best available way to calibrate the cloud water retrieval.
Cloud PDF (1/mm)
Cloud PDF (1/mm)
Cloud PDF (1/mm)
0.0 0.1 0.2 0.3 0.4
Fig. 10. Probability density functions (pdf) for liquid cloud water. The cloud pdf’s are
stratified according to sea-surface temperature, wind speed, and water vapor. Each
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